RAC Operations Manual Part ABD.pdf - Redcliffe Aero Club

© AEROSERVICE 2000

08/00 i

THE REDCLIFFE AERO CLUB

OPERATIONS MANUAL

CHARTER AND AERIAL WORKOPERATIONS

for

AEROPLANES NOT EXCEEDING5700 Kg MTOW


© AEROSERVICE 2000

08/00 OPERATIONS MANUAL ii

THIS PAGE INTENTIONALLY LEFT BLANK


© AEROSERVICE 2000 AMD 4

06/02 OPERATIONS MANUAL iii

L AUTHORITY

This Operations Manual derives its authority from Regulation 215 of the Civil Aviation

Regulations and is provided for the sole use and guidance of the operations personnel of -


ABN 74 009 819 792

PO BOX 26

KIPPA-RING QLD 4021

PUBLISHER'S NOTE AND COPYRIGHT

(1) This Operations Manual has been prepared in accordance with the Civil Aviation

Advisory Publication 215(1)(0) 'Guide to the Preparation of Operations Manuals'

and is produced and published by;

AEROSERVICE PUBLICATIONS PTY LTD

74 Pioneer Road

Sheldon

Queensland, 4157.

Phone/Fax: 07 3206 4288

L Email: [email protected]

(2) Every possible effort has been made to establish the accuracy of the information

and instructions contained in this document, but the publisher accepts no

responsibility or liability for errors or omissions and users are hereby advised that

nothing contained herein must be implied, understood or applied in contradiction to

the Civil Aviation Regulations or any other law of the Commonwealth of Australia

or of the Parliament of any Australian State.

(3) This Operations Manual shall not, by way of trade or otherwise, be lent, resold,

hired out or otherwise circulated, or copied, or reprinted, or reproduced by any other

means whatsoever without prior written permission from the publisher.



03/06 OPERATIONS MANUAL iv

DISTRIBUTION

A copy of this Operations Manual shall be issued to all operating crew members employed

by the Club

All persons who are issued with a copy of this Club Operations Manual will be held solely

responsible for the security and safe keeping of that copy and must ensure that:

(a) It is not given into the hands of any unauthorised person; and

(b) No part of the material contained therein is used for other than the Club's own

operational purposes.

After each Manual is issued the Chief Pilot shall record, in the table below in Copy No 2,

the Copy number, the composition of the particular Manual and the name of the Manual

holder to whom the particular Manual is issued.

COPY NOPART

MANUAL HOLDERA B C D E INDEX

1 U U U U U CASA

L 2 U U U U U Library/Briefing Area

L 3 U U U U U Chief Pilot/CFI/Master Copy

4 U U U U U

5 U U U U U

6 U U U U U

7 U U U U U

8 U U U U U

9

10



04/04 OPERATIONS MANUAL v

SIGNATURE SHEET/1

COMPLIANCE REQUIREMENT

(1) The instructions, procedures and information contained in this manual have been

devised to ensure safety and standardisation in the conduct of Club operations.

They are to be observed by all operating personnel who are reminded of their

obligation to comply with the Civil Aviation Act, CARs, CAOs and such other

directives, aeronautical information and notices that the CASA may publish from

time to time.

(2) Where, in the light of operating experience, errors are found in the manual or

deficiencies in the manner in which THE REDCLIFFE AERO CLUB operations are

conducted, recommendations for amendment shall be submitted to the Chief Pilot.

Instruction:

(1) All Club personnel associated with piloting and flight line management must sign

this sheet in the library copy as evidence of having read, understood and agreed

to apply the procedures and data contained in this Operations Manual.

L (2) Each person required to sign, including trainee pilots, must do so on joining the

Club and at intervals not exceeding twelve months and when an amendment has

been made.

PRINTED NAME SIGNATURE DATE


© AEROSERVICE 2000

08/00 OPERATIONS MANUAL vi

SIGNATURE SHEET/2



© AEROSERVICE 2000

OPERATIONS MANUAL

SIGNATURE SHEET/3



© AEROSERVICE 2000

OPERATIONS MANUAL

SIGNATURE SHEET/4



© AEROSERVICE 2000

OPERATIONS MANUAL

SIGNATURE SHEET/5



© AEROSERVICE 2000

OPERATIONS MANUAL

SIGNATURE SHEET/6




03/09 OPERATIONS MANUAL vii

LIST OF EFFECTIVE PAGES

* This check list applies to those pages which comprise the Club Operations Manual up

to and including Amendment No. 15, dated 27 March, 2009.

* The date code shown against each page indicates the month/year of issue. Any changes

affecting this Manual will be executed by an Operations Manual amendment issued to

all Manual holders and will be accompanied by an updated list of effective pages.

* Amended text will be indicated by the symbol L in the margin adjacent to the beginning

of the paragraph containing the amended text.

* IT IS THE RESPONSIBILITY OF THE CHIEF PILOT TO ENSURE ALL COPIES OF

THIS MANUAL ARE MAINTAINED IN A CURRENT STATUS.

Page Date Page Date Page Date Page Date

No Code No Code No Code No Code

i 08/00ii 08/00iii 06/02iv 03/06v 04/04vi 08/00vii 03/09viii 03/09ix 03/09x 03/09xi 03/09xii 03/09Master AmendmentRecord (MasterCopy only) 08/00xiii 08/00xiv 08/00xv 08/00A(i) 08/00A(ii) 08/00A(iii) 04/04AO-1 11/05AO-2 08/00AO-3 11/05AO-4 04/04AO-5 04/04AO-6 04/04AO-7 01/05AO-8 01/05AO-9 04/04AO-10 04/04AO-11 04/04

AO-12 01/05AO-13 08/00AO-14 04/04AO-15 08/07AO-16 08/00AO-17 08/00AO-18 04/04AO-19 08/00AO-20 08/00AO-21 08/00AO-22 08/00AO-23 08/00Appendix 1Page 1 04/04Appendix 2Page 1 11/05Page 2 11/05A1-1 08/00A1-2 06/02A1-3 08/00A1-4 03/09A1-5 08/07A1-6 08/07A1-7 08/07A1-8 08/07A1-8a 08/07A1-8b 08/07A1-9 08/00A1-10 04/04A1-11 08/00A1-12 04/04A1-13 04/04

A1-14 04/04A1-15 08/00A1-16 08/00A1-17 06/02A1-18 03/09A1-19 03/09A1-20 03/09A1-21 06/02A1-22 06/02A1-23 06/02A1-24 06/02A1-25 06/02A1-26 06/02A1-27 06/02A1-28 06/02Appendix 1Page 1 08/00Appendix 2Page 1 08/00Appendix 3Page 1 03/09Page 2 03/09Page 3 08/07Appendix 4Page 1 03/09Page 2 03/09Appendix 5Page 1 08/00Page 2 08/00A2-1 01/05A2-2 03/06A2-3 08/00

A2-4 08/07A2-5 06/02A2-6 03/09A2-7 08/00A2-8 08/00A2-9 08/00A2-10 08/00A2-11 06/02A2-12 08/00A2-13 03/06A2-14 03/06A2-15 08/00A2-16 01/05A2-17 03/06Appendix 1Page 1 08/00Page 2 01/05Appendix 2Page 1 04/04Appendix 3Page 1 03/09Appendix 4Page 1 01/05Appendix 5Page 1 08/00Appendix 6Page 1 03/09Appendix 7Page 1 03/09A3-1 01/05A3-2 04/04A3-3 06/02

03/09 OPERATIONS MANUAL viii


Page Date Page Date Page Date Page DateNo Code No Code No Code No Code



A3-4 06/02A3-5 08/07A3-6 03/06A3-7 08/00A3-8 08/07A3-9 08/07A3-10 08/07A3-11 10/00A3-12 08/07A3-13 08/07A3-14 08/07A3-15 06/02A3-16 08/00A3-17 10/00A3-18 04/04A3-19 08/07A3-20 03/06Appendix 1Page 1 08/00Appendix 2Page 1 08/00Appendix 3Page 1 01/05Page 2 01/05Appendix 4Page 1 01/05Page 2 10/00Page 3 01/05Appendix 5Page 1 04/04Appendix 6Page 1 04/04A4-1 10/00A4-2 04/04A4-3 08/00A4-4 08/00A4-5 04/04A4-6 06/08A4-7 06/08A4-7a 06/08A4-7b 06/08A4-8 04/04A4-9 04/04A4-10 04/04A4-11 04/04A4-12 04/04A4-13 04/04Appendix 1Page 1 08/00

Appendix 2Page 1 08/00A5-1 08/00A5-2 08/00A5-3 04/04A5-4 08/00A5-5 08/00A5-6 08/00A5-7 08/00A5-8 10/00A5-9 06/02A5-10 08/00A5-11 08/00A5-12 08/00A5-13 08/00A5-14 06/08A5-15 08/00A5-16 08/00A5-17 08/00A5-18 08/00A5-19 08/00A5-20 08/00A5-21 08/00A5-22 08/00Appendix 1Page 1 08/00A6-1 08/00A6-2 06/02A6-3 03/06A6-4 03/06A6-5 06/02A6-6 06/02A6-7 06/02A6-8 08/00A6-9 08/00A6-10 08/00A6-11 04/04A6-12 04/04A6-13 08/00A6-14 08/00A6-15 04/04A6-16 03/06A6-17 08/00A6-18 08/00A6-19 08/00A6-20 04/04A6-21 08/00A6-22 08/07A6-22a 08/07

A6-22b 08/07A6-23 08/00A6-24 08/00A6-25 03/06A6-26 04/04A6-27 08/00A6-28 08/00A6-29 08/00Appendix 1Page 1 08/00Appendix 2Page 1 03/06Page 2 01/09Page 3 08/00Page 4 08/00Page 5 08/00Page 6 08/00Page 7 08/00Page 8 08/00Page 9 08/00Page 10 08/00Page 11 08/00 08/00Page 13 08/00Page 14 08/00Page 15 08/00Page 16 08/00Page 17 08/00Page 18 08/00Page 19 08/00Page 20 08/00Page 21 10/00Page 22 10/00Page 23 08/00Page 24 08/00Page 25 08/00Page 26 08/00Page 27 08/00Page 28 08/00Page 29 08/00Page 30 08/00Page 31 08/00Page 32 08/00Page 33 08/00Page 34 08/00Page 35 08/00Page 36 08/00Page 37 08/00Page 38 08/00

Page 39 08/00Page 40 08/00Page 41 08/00Page 42 08/00Page 43 08/00Page 44 08/00Page 45 08/00Page 46 08/00Page 47 04/04Page 48 04/04Page 49 06/02Page 50 04/04Page 51 06/02Page 52 04/04Page 53 06/02Page 54 06/02Page 55 04/04Page 56 06/02Page 57 06/02Page 58 04/04Page 59 06/02Page 60 06/02Page 61 06/02Page 62 04/04Page 63 12/02Page 64 12/02Page 65 12/02Page 66 12/02Page 67 12/02Page 68 12/02Page 69 01/03Page 70 01/03Page 71 01/03Page 72 01/03Page 73 01/05Page 74 01/05Page 75 01/05Page 76 01/05Page 77 11/05Page 78 11/05Page 79 11/05Page 80 11/05Page 81 11/05Page 82 11/05Page 83 08/07Page 84 08/07Page 85 08/07Page 86 08/07Page 87 08/07

03/09 OPERATIONS MANUAL ix





Page 88 08/07Page 89 08/07Page 90 08/07Page 91 08/07Page 92 08/07Page 93 08/07Page 94 08/07Page 95 08/07Page 96 08/07Page 97 08/07Page 98 08/07Page 99 08/07Page 100 08/07Page 101 08/07Page 102 08/07Page 103 08/07Page 104 08/07Page 105 08/07Page 106 08/07Page 107 08/07Page 108 08/07Page 109 08/07Page 110 08/07Page 111 06/08Page 112 06/08Page 113 06/08Page 114 06/08Page 115 06/08Page 116 06/08Page 117 01/09Page 118 01/09Page 119 01/09Page 120 01/09Page 121 01/09Page 122 01/09Page 123 01/09Page 124 01/09Page 125 01/09Page 126 01/09Page 127 01/09Page 128 01/09Page 129 01/090 01/09Page 131 01/09Page 132 01/09Page 133 01/09Page 134 01/09Page 135 01/09Page 136 01/09

Appendix 3Page 1 04/04Page 2 04/04Page 3 04/04Appendix 4Page 1 08/07Page 2 08/07A7-1 04/04A7-2 04/04A7-3 04/04A7-4 04/04A7-5 04/04A7-6 04/04A7-7 04/04A7-8 04/04A7-9 04/04Appendix 1Page 1 04/04Appendix 2Page 1 04/04Appendix 3Page 1 04/04Appendix 4Page 1 04/04A8-1 03/06A8-2 03/06A8-3 03/06A8-4 08/07A8-5 08/07A8-6 03/06A8-7 03/06A8-8 03/06A8-9 03/06A8-10 03/06A8-11 03/06A8-12 03/06Appendix 1Page 1 01/09Page 2 01/09Page 3 01/09Page 4 01/09Page 5 01/09Page 6 01/09Appendix 2Page 1 04/04Appendix 3Page 1 01/09Page 2 01/09Appendix 4

Page 1 04/04Appendix 5Page 1 01/09Page 2 01/09Appendix 9Page 1 08/07A10-1 03/09A10-2 03/09A10-3 03/09A10-4 03/09A10-5 03/09A10-6 03/09A10-7 03/09A10-8 03/09A10-9 03/09A10-10 03/09A10-11 03/09A10-12 03/09A10-13 03/09A10-14 03/09A10-15 03/09A10-16 03/09A10-17 03/09A10-18 03/09A10-19 03/09A10-20 03/09A10-21 03/09A10-22 03/09A10-23 03/09A10-24 03/09Appendix 1Page 1 03/09Appendix 2Page 1 03/09Page 2 03/09Appendix 3Page 1 03/09Appendix 4Page 1 03/09Appendix 5Page 1 03/09

PART BAEROPLANES

A-B(i) 08/00A-B(ii) 08/00A-B(iii) 08/00A-BO-1 08/00

A-BO-2 08/00A-BO-3 08/00A-B1-1 04/04A-B1-2 08/00A-B1-3 03/06A-B1-4 08/00A-B1-5 03/06A-B1-6 08/00A-B1-7 04/04A-B1-8 04/04A-B1-9 04/04A-B1-10 03/06A-B2-1 08/00A-B2-2 08/00A-B2-3 08/00A-B2-4 08/00Appendix 1Page 1 01/09A-B5-1 08/07A-B5-2 08/00A-B5-3 08/07A-B5-4 08/07A-B5-5 08/07

PART DD(i) 08/00D(ii) 08/00D(iii) 08/00DO-1 08/00DO-2 08/00DO-3 08/00DO-4 08/00DO-5 08/00D1-1 08/00D1-2 08/00D1-3 08/00Appendix 1Page 1 08/00D2-1 08/00D2-2 08/00D3-1 08/00D3-2 08/00D3-3 08/00D4-1 08/00D4-2 08/00D4-3 08/00D4-4 08/00D5-1 08/00D5-2 08/00

03/09 OPERATIONS MANUAL x





D6-1 08/00D6-2 08/00D6-3 08/00

INDEXIDX-1 03/09IDX-2 03/09IDX-3 03/09IDX-4 03/09IDX-5 03/09IDX-6 03/09IDX-7 03/09IDX-8 03/09IDX-9 03/09

PART EE(i) 08/00E(ii) 08/00E(iii) 06/02E(iv) 08/00E(v) 08/00

SECTION EOEO-1 08/00EO-2 08/00EO-3 08/00

SECTION E1E1-1 08/00E1-2 08/00E1-3 08/00E1-4 08/00E1-5 08/00E1-6 08/00E1-7 10/00E1-8 10/00

SECTION E2E2-1 03/09E2-2 03/09E2-2a 06/02E2-2b 06/02E2-3 06/02E2-4 08/00E2-5 06/08E2-6 08/00E2-7 08/00E2-8 06/02E2-9 08/00

E2-10 08/00E2-11 06/02E2-12 06/08E2-13 08/00E2-14 08/00E2-15 03/09E2-16 03/09E2-17 08/00E2-18 08/00E2-19 10/00E2-20 03/09Appendix 1Page 1 04/04Appendix 2Page 1 08/00Appendix 3Page 1 08/00Page 2 08/00Page 3 08/00Page 4 08/00Page 5 08/00Appendix 4Page 1 08/00Appendix 5Page 1 08/00Page 2 08/00Appendix 6Page 1 08/00Appendix 7Page 1 03/06Page 2 03/06

SECTION E3E3(i) 06/08

Sub-section 3.0E3.0-1 08/00E3.0-2 08/00E3.0-3 08/00E3.0-4 08/00E3.0-5 08/00E3.0-6 08/00E3.0-7 08/00E3.0-8 08/00E3.0-9 08/00E3.0-10 08/00E3.0-11 08/00E3.0-12 08/00E3.0-13 08/00

E3.0-14 08/00E3.0-15 08/00E3.0-16 08/00E3.0-17 02/01E3.0-18 02/01E3.0-19 02/01E3.0-20 02/01E3.0-21 08/00

Sub-section 3.1E3.1-1 08/00E3.1-2 08/00E3.1-3 08/00E3.1-4 08/00E3.1-5 08/00E3.1-6 08/00E3.1-7 08/00E3.1-8 08/00E3.1-9 08/00E3.1-10 08/00E3.1-11 02/01E3.1-12 02/01E3.1-13 02/01E3.1-14 02/01E3.1-15 02/01E3.1-16 02/01E3.1-17 02/01E3.1-18 02/01E3.1-19 02/01E3.1-20 02/01E3.1-21 02/01E3.1-22 02/01E3.1-23 02/01E3.1-24 02/01E3.1-25 02/01E3.1-26 02/01E3.1-27 02/01E3.1-28 02/01E3.1-29 02/01E3.1-30 02/01E3.1-31 02/01E3.1-32 02/01E3.1-33 02/01E3.1-34 02/01

Sub-section 3.2E3.2-1 08/00E3.2-2 08/00E3.2-3 02/01

E3.2-4 02/01E3.2-5 02/01E3.2-6 02/01E3.2-7 02/01E3.2-8 02/01E3.2-9 02/01E3.2-10 02/01E3.2-11 02/01E3.2-12 02/01E3.2-13 02/01E3.2-14 02/01

Sub-section 3.3E3.3-1 08/00E3.3-2 08/00E3.3-3 08/00E3.3-4 08/00E3.3-5 08/00

Sub-section 3.4E3.4-1 08/00E3.4-2 08/00E3.4-3 08/00E3.4-4 08/00E3.4-5 02/01E3.4-6 02/01E3.4-7 02/01E3.4-8 02/01E3.4-9 02/01E3.4-10 02/01E3.4-11 02/01E3.4-12 02/01E3.4-13 02/01E3.4-14 02/01E3.4-15 02/01E3.4-16 02/01E3.4-17 02/01E3.4-18 02/01E3.4-19 02/01E3.4-20 02/01E3.4-21 02/01E3.4-22 02/01E3.4-23 02/01

Sub-section 3.8E3.8-1 08/00E3.8-2 08/00E3.8-3 08/00E3.8-4 08/00

03/09 OPERATIONS MANUAL xi





E3.8-5 08/00E3.8-6 08/00E3.8-7 08/00E3.8-8 08/00E3.8-9 08/00E3.8-10 08/00E3.8-11 08/00E3.8-12 08/00E3.8-13 08/00E3.8-14 08/00E3.8-15 08/00E3.8-16 08/00E3.8-17 08/00

Sub-section 3.10E3.10-1 08/00E3.10-2 08/00E3.10-3 08/00E3.10-4 08/00E3.10-5 08/00E3.10-6 08/00E3.10-7 08/00E3.10-8 08/00

Sub-section 3.11E3.11-1 03/09E3.11-2 03/09E3.11-3 03/09E3.11-4 03/09E3.11-5 03/09E3.11-6 03/09E3.11-7 03/09E3.11-8 03/09E3.11-9 03/09E3.11-10 03/09E3.11-11 03/09E3.11-12 03/09E3.11-13 03/09E3.11-14 03/09E3.11-15 03/09E3.11-16 03/09E3.11-17 03/09E3.11-18 03/09E3.11-19 03/09E3.11-20 03/09E3.11-21 03/09E3.11-22 03/09E3.11-23 03/09E3.11-24 03/09

E3.11-25 03/09E3.11-26 03/09E3.11-27 03/09Appendix 1Page 1 03/06Page 2 03/06Page 3 03/06Appendix 2Page 1 03/09Page 2 03/09

Sub-section 3.12E3.12-1 12/00E3.12-2 12/00E3.12-3 12/00E3.12-4 12/00E3.12-5 12/00E3.12-6 12/00E3.12-7 12/00E3.12-8 12/00E3.12-9 12/00E3.12-10 12/00E3.12-11 12/00E3.12-12 12/00E3.12-13 12/00E3.12-14 12/00E3.12-15 12/00E3.12-16 12/00E3.12-17 12/00E3.12-18 12/00E3.12-19 12/00E3.12-20 12/00

Sub-section 3.14E3.14-1 08/00E3.14-2 08/00E3.14-3 08/00E3.14-4 08/00E3.14-5 08/00E3.14-6 08/00E3.14-7 08/00

Sub-section 3.15E3.15-1 08/00E3.15-2 08/00E3.15-3 08/00E3.15-4 08/00

Sub-section 3.16

E3.16-1 08/00Appendix 1Page 1 08/00

Sub-section 3.20E3.20-1 03/09E3.20-2 12/00E3.20-3 12/00E3.20-4 12/00E3.20-5 06/02E3.20-6 06/02E3.20-7 06/02E3.20-8 06/02E3.20-9 06/02E3.20-10 06/02E3.20-11 06/02E3.20-12 06/02E3.20-13 06/02E3.20-14 06/02E3.20-15 06/02E3.20-16 06/02E3.20-17 06/02E3.20-18 06/02E3.20-19 06/02E3.20-20 06/02E3.20-21 06/02E3.20-22 06/02E3.20-23 06/02E3.20-24 06/02E3.20-25 06/02E3.20-26 06/02E3.20-27 06/02Appendix 1Page 1 12/00Page 2 12/00Page 3 06/02Page 4 06/02Page 5 06/02Page 6 06/02Page 7 06/02Page 8 06/02Page 9 06/02Page 10 06/02Page 11 06/02Page 12 06/02

Sub-section 3.22E3.22-1 04/04E3.22-2 04/04E3.22-3 04/04E3.22-4 04/04

Sub-section 3.23E3.23-1 03/06E3.23-2 03/06E3.23-3 03/06E3.23-4 03/06E3.23-5 03/06E3.23-6 03/06E3.23-7 03/06E3.23-8 03/06E3.23-9 03/06E3.23-10 03/06Appendix 1Page 1 03/06

Sub-section 3.24E3.24-1 03/06E3.24-2 03/06E3.24-3 03/06E3.24-4 03/06E3.24-5 03/06Appendix 1Page 1 03/06

Sub-section 3.25E3.25-1 06/08E3.25-2 06/08E3.25-3 06/08E3.25-4 06/08E3.25-5 06/08

Sub-section 3.26E3.26-1 03/09E3.26-2 03/09E3.26-3 03/09E3.26-4 03/09E3.26-5 03/09E3.26-6 03/09E3.26-7 03/09E3.26-8 03/09E3.26-9 03/09E3.26-10 03/09

SECTION E4

03/09 OPERATIONS MANUAL xii





E4-1 10/00E4-2 08/00E4-3 12/00E4-4 08/00E4-5 10/00E4-6 12/00E4-7 10/00E4-8 10/00Appendix 1Page 1 08/00Appendix 2Page 1 08/00Appendix 3Page 1 08/00Appendix 4Page 1 04/04


© AEROSERVICE 2000

08/00 OPERATIONS MANUAL xiii AMENDMENT RECORD

Amendment ACTIONED BY DATEACTIONEDNo. Date Name Signature

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© AEROSERVICE 2000

08/00 OPERATIONS MANUAL xiv

AMENDMENT RECORD

Amendment ACTIONED BY DATEACTIONEDNo. Date Name Signature

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© AEROSERVICE 2000

08/00 OPERATIONS MANUAL xv

INDEX TO PARTS

PART A: GENERAL OPERATING PROCEDURES

PART B: SPECIFIC AIRCRAFT OPERATING PROCEDURES

PART C: RESERVED

PART D: SPECIALISED OPERATIONS

PART E: FLYING SCHOOL OPERATIONS

© AEROSERVICE 2000

08/00 A(i)


OPERATIONS MANUAL

PART A

GENERAL OPERATING PROCEDURES


© AEROSERVICE 2000

08/00 OPERATIONS MANUAL A(ii)




04/04 OPERATIONS MANUAL A(iii)

PART A

GENERAL OPERATING PROCEDURES

INDEX TO SECTIONS

TITLE SECTION

PREFACE PAGES AO

GENERAL A1

FLIGHT CREW ADMINISTRATION A2

AIRCRAFT ADMINISTRATION A3

PASSENGER AND FREIGHT ADMINISTRATION A4

EMERGENCY PROCEDURES A5

FLIGHT CONDUCT A6

L SAFETY MANAGEMENT AND AUDITING A7

L DANGEROUS GOODS ADMINISTRATION A8



11/05 OPERATIONS MANUAL AO-1

SECTION AO

PREFACE PAGES

SUB-SECTION PAGE

0.1 INTRODUCTION AO-3

0.2 DEFINITIONS AND ABBREVIATIONS AO-5

0.3 CARs AND CASRs RELEVANT TO CLUB OPERATIONS AO-8

0.4 CARs AND THE FLIGHT CREW MEMBER AO-13

0.5 CAOs RELEVANT TO CLUB OPERATIONS AO-15

0.6 CONVERSION TABLES AO-17

APPENDIXES

1. ERRATUM/REQUEST FOR CHANGE REPORT

L 2. AMENDMENT LIST AND AMENDMENT CERTIFICATION


© AEROSERVICE 2000

08/00 PREFACE PAGES AO-2





0.1 INTRODUCTION

(1) The object of the Club Operations Manual is to reflect Club policy and outlinethe operational requirements, procedures and general principles by which THE

REDCLIFFE AERO CLUB aims to achieve and maintain a level of standardisationthat will ensure maximum safety and efficiency of its flight operations.

(2) 'Notes' and 'Warnings' where used are for the purpose of emphasising specificprocedures, instructions or information about an operational condition,procedure, or technique which it is considered necessary to emphasise in theinterests of safety.

(3) Each member of this organisation associated with the administration,operation, servicing and piloting of Club operated aircraft shall comply with allinstructions contained in the Operations Manual in so far as they relate to thatperson's duties and responsibilities.

(4) This Operations Manual will be revised from time to time to ensure continuedcompliance with the Civil Aviation Act, CARs, CAOs, AIP and such otherdirectives which may be issued by the Civil Aviation Safety Authority or, whereit is considered necessary in the light of operational experience, to reflectchanges in Club operations or equipment.

L (5) Operations Manual Amendments shall be issued in numerical order and areto be incorporated in all copies of the Club’s Operations Manual. EachAmendment shall include an Amendment List, identifying the additions,changed sheets and deletions, and an Amendment Certification. Amendedpages shall be inserted as soon as possible after receipt, or if an effectivedate is published, on that date. Entries in relation to the Amendment shall beentered in the Amendment Record at Page xi in each Operations Manual bythe person completing that Amendment. The person completing theAmendment shall also complete the Amendment Certification and return it tothe Chief Pilot. Samples of the Amendment List and the AmendmentCertification are shown at Appendix 2 to this Section.

(6) A copy of each such Amendment must be forwarded to the appropriate officeof the Civil Aviation Safety Authority. When the amendment involves anaddition or any other variation to the organisation's Air Operators' Certificate,that amendment shall be supported by a suitable written application. Thisapplication shall, where possible, be submitted to the appropriate CASAService Centre 90 days before the Club proposes to commence operations.

....




0.1 INTRODUCTION

L (7) Club personnel are encouraged to submit suggestions for changes to

Operations Manual procedures and/or content to the Chief Pilot. No change

in procedures shall be implemented until published by a Notice or an

Amendment to the Operations Manual.

(8) Persons in the employ of THE REDCLIFFE AERO CLUB, are required not to

divulge any information about the business of THE REDCLIFFE AERO CLUB that

the employee gains, has, or becomes privy to while in the employ of THE

REDCLIFFE AERO CLUB or details of operations of THE REDCLIFFE AERO CLUB to

any media outlet, person or business, whether that person or business be in

competition or not, either directly or indirectly with THE REDCLIFFE AERO CLUB.

L (9) Club personnel are required to inform the Chief Pilot of any error,

misinformation or superseded data noted in this Operations Manual. Staff are

also encouraged to submit suggestions for changes to procedures and/or

content of this Operations Manual to the Chief Pilot. Club staff shall utilise the

“ERRATUM/REQUEST FOR CHANGE REPORT” for this notification. No change in

procedures shall be implemented until published by an Amendment to the

Operations Manual. A copy of the Erratum/Request for Change Report is

shown at Appendix 1 to this Section.

0.2 DEFINITIONS AND ABBREVIATIONS

* For official definitions consult the Civil Aviation Regulations and the AIP.

* Aviation terms and expressions used in this Operations Manual, unless

otherwise defined shall have the same meaning and/or interpretation and/or

explanations given in the Civil Aviation Regulations, Civil Aviation Orders and

the AIP.

In addition to the above the following definitions and abbreviations will apply without

prejudice in the context of this Operations Manual:

Club, School, Organisation or Operator means -


....





Management means the Club administration and includes any person who is

responsible for managing, directing or controlling Club affairs.

Civil Aviation Act means the Civil Aviation Act 1988 which establishes a Civil

Aviation Safety Authority with functions relating to the safety of civil aviation and for

related purposes.

Air Services Act means the Air Services Act 1996 which establishes Airservices

Australia with functions relating to the control of civil aviation in Australia and for

related purposes.

Civil Aviation Safety Authority means the Australian Civil Aviation Safety Authority

established by the Civil Aviation Act 1988. CASA has a corresponding meaning.

L Civil Aviation Regulations means the Civil Aviation Regulations 1988 and the

Civil Aviation Safety Regulations 1998 of Australia that are in force under the Civil

Aviation Act, and as amended from time to time by Statutory Rules. CAR, CARs,

CASR or CASRs has a corresponding meaning.

Civil Aviation Orders means orders issued by the Civil Aviation Safety Authority

pursuant to the Civil Aviation Regulations. CAO or CAOs has a corresponding

meaning.

Aeroplane Landing Area/ALA means any place other than a place referred to in

paragraph (a), (b) or (c) of CAR 92(1) which is suitable for use as an aerodrome for

the purposes of the landing and taking-off of land aeroplanes.

Charter Operations in the context of the Club's operations means the use of a

aeroplane for the carriage of passengers and cargo, other than Club employees and

cargo owned by the Club, to and from any place. The passengers so carried are

required be covered by Compulsory Passenger Liability Insurance as required by the

Civil Aviation (Carriers' Liability) Act 1959, as amended.

Aerial Work Operations in the context of the Club's operations means the use of a

Club aeroplane in specialised operations for which detailed operating procedures are

contained in Part D of this Operations Manual. Any person carried shall have duties

which are essential to the successful conduct of the operation. The persons carried will

not be covered by Compulsory Passenger Liability Insurance.

....





Private Operations in the context of the Club's operations means the use of a Clubaeroplane for the carriage of Club employees and cargo owned by the Club, to andfrom any place.

Chief Pilot means the person nominated by the Club and approved by the CivilAviation Safety Authority to supervise the conduct of Club flying operations.

Chief Flying Instructor means a rated flight instructor nominated by the Club andapproved by the Civil Aviation Safety Authority to give practical flight instruction,supervise the duties of other flight instructors employed by the Club and ensure thatflying training operations are conducted in accordance with the Club OperationsManual. CFI has the same meaning.

Pilot in Command means the pilot responsible for the operation and safety of anaircraft during flight including all associated pre-flight and post flight activities.

Operating Crew or Crew Member means any person having duties on boardwhich are essential to the successful conduct of the operation, the flying or safetyof the flight of that aircraft.

Student Pilot means a person receiving practical flight instruction to increase his/herskill to the standard required for the issue of a pilot licence of a higher category.

Check Flight means any periodic proficiency test or any other flight check carriedout by the Chief Pilot or other approved person to test the competency of the Club'sflight crew members.

Passenger means any person on board an aircraft other than an Operating Crewor Crew Member rostered for that flight, engineers on board for flight test purposesand CASA personnel on official duties.

Adult in the context of this manual, means a passenger 13 years of age and over.

Child, in the context of this manual, means a passenger who has reached his/herthird birthday but not his/her thirteenth birthday. Children has a correspondingmeaning.

Infant means a passenger who has not reached his/her third birthday.

Handicapped Person means a person requiring special attention or assistancebecause of illness, injury, age, congenital malfunction, or other temporary orpermanent incapacity or disability.

....





Animals in the context of the Club's operations, means any member of the animalkingdom (other than man) including mammals, birds, reptiles, fish, insects,crustaceans and shell-fish.

Cargo or Goods means all things other than persons carried in the aircraft.

L Dangerous Goods means all substances that come under the general heading ofdangerous goods as defined in Sub-section 23(3) of the Civil Aviation Act andamplified in Civil Aviation Safety Regulation 92.015 and the ICAO TechnicalInstructions for the Safe Transport of Dangerous Goods by Air..

Operations Manual means the Club's Operations Manual comprising Parts A, B,D and E.

Flight Manual means the Flight Manual as defined in CAR 54 and includes anyalterations made from time to time.

Manufacturer's Handbook means the Pilot's Operating Handbook or similardocument produced by the aircraft manufacturer for a specified model of a particulartype of aircraft and containing the operating procedures and other data required bythe pilot for the safe and efficient operation of that aircraft. This document may ormay not form part of the Aircraft Flight Manual.

Time in Service for the purpose of entries in the aircraft's Maintenance Release iscalculated from the aeroplane's "WHEELS OFF" to "WHEELS ON" for each flight.

Flight Time for the purposes of the pilot's flight crew logbook and Flight and DutyTime records is defined as "BLOCK TIME", the elapsed time from when theaeroplanes first starts to move under its own power for the purpose of a flight untilthe moment at which the aeroplane comes to a rest on completion of the flight.




0.3 CARs and CASRs RELEVANT TO CLUB OPERATIONS

The Civil Aviation Act 1988 requires compliance with the Act and Civil Aviation

Regulations in force under the Act. While all CARs are relevant and must be

complied with, the following regulations are of particular significance to Club

operations.

L CIVIL AVIATION REGULATIONS 1988

APPLICATION, ADMINISTRATION & ORGANISATION

3 Application of Regulations

5 Civil Aviation Orders

6 Authorised persons

REGISTRATION OF AIRCRAFT

10 Application for registration

13D Acquisition and disposal of interests

CERTIFICATES OF APPROVAL AND AIRCRAFT MAINTENANCE ENGINEER

LICENCES

30 Certificates of approval

32 Period of operation of certificates and licences

MISCELLANEOUS

37 Permissible unserviceabilities

MAINTENANCE

41 Maintenance schedule and maintenance instruction

42 Defective or inappropriate maintenance schedule

42G Flight control system - additional requirements

42ZC Maintenance on Australian aircraft in Australian territory

42ZE Certification of completion of maintenance on Australian aircraft

43 Maintenance Releases in respect of Australian aircraft

....





MAINTENANCE

43B Flight time to be recorded on Maintenance Release

44 Conditions with respect to Maintenance Releases

45 Suspension or cancellation of Maintenance Release

46 Information to be passed to other persons

47 Maintenance Release to cease to be in force

48 Maintenance Release to recommence to be in force

50 Defects and major damage to be endorsed on Maintenance Release

50Ato Aircraft log books50D

51to Defect reporting/Investigation53

54 Meaning of flight manuals

55 Changes to flight manuals for Australian aircraft

QUALIFICATIONS OF FLIGHT CREW

5.04 Medical certificates - flight crew licences

5.08 to Flight crew licences - application, issue, duration and conditions5.265.40 Pilot acting in command under supervision

5.59 Flight crew licence - syllabuses of training

5.60 Instrument ground time - approval of trainer

AERODROMES AND FACILITIES AND SERVICES

92 Use of aerodromes, etc.

METEOROLOGICAL SERVICES

120 Weather reports not to be used unless made with authority....





STATISTICAL RETURNS

132 Statistical returns

CONDITIONS OF FLIGHT

133 Conditions to be met before Australian aircraft may flyL

139 Documents to be carried in Australian aircraft

140 Prohibited, restricted and danger areas

143 Carriage of firearms

150 Dropping of articles

153 Flight under simulated conditions

155 Acrobatic flight

157 Low flying

AIR SERVICE OPERATIONS

206 Commercial purposes

207 Requirements according to operations on which aircraft used

208 Number of operating crew

209 Private operations

REQUIREMENTS TO ENSURE THE SAFETY OF COMMERCIAL OPERATIONS

212 Operator

213 Organisation

214 Training of maintenance personnel

215 Operations Manual

216 Flight time records

219 Route qualifications of pilot in command of a charter aircraft

220 Fuel instructions and records

221 Facilities and safety devices for public ....





CONDUCT OF OPERATIONS

224 Pilot in command

252 Provision of emergency equipment

226 Dual controls

229 Aircraft not to be taxied except by pilot or person approved for thepurpose

230 Starting and running of aircraft engines

232 Flight check system

234(2) Fuel requirements

235 Takeoff and landing of aircraft

235A Minimum runway width

248(2) Action in relation to defects

GENERAL PROVISIONS RELATING TO THE OPERATION OF AIRCRAFT

249 Prohibition of carriage of passengers on certain flights

250 Carriage on wings, undercarriage etc.

251 Seat belts and safety harness

252 Provision of emergency equipment

253 Emergency and life saving equipment

255 Smoking in aircraft

256 Intoxicated persons not to act as pilots, etc., or be carried in aircraft

256A Carriage of animals

262 Carriage of examiners (Flying Operations Inspectors)L

PENAL PROVISIONS AND PROSECUTIONS

281 to Penal Provisions295

....





MISCELLANEOUS

299 Change of address

301 Surrender of documents

302 Production of licences, etc.

305 Access of authorised person to aerodromes, aircraft, etc.

309A Instructions about activities on board aircraft

CIVIL AVIATION SAFETY REGULATIONS 1998

21.2C Suspension or cancellation of an instrument

21.5 Aeroplane or rotorcraft flight manual

21.175 Certificates of airworthiness: classification

21.197 Special fight permits

39 Airworthiness directives

45 Nationality, Registration and identification

92.015 What are dangerous goods?

92.025 Compliance with Technical Instructions - operators

L 92.030 Compliance with Technical Instructions - passengers and crew

92.070 Dangerous Goods Statement

92.095 Training - certain employees of Australian operators

92.110 Required standard of training for 92.095

92.140 Who may conduct training

92.145 Records about training

92.175 Goods carried by private operators


© AEROSERVICE 2000


0.4 CARs AND THE FLIGHT CREW MEMBER

A flight crew member, in the course of his/her duties, is required to comply with Civil

Aviation Regulations and the CAOs, AIPs, NOTAMs and other directives that derive

authority from the CARs. This includes compliance with:

5.01 to

The general requirements for licence(s) and ratings

5.26and various conditions associated with the licence(s)

5.51 to Personal log books, recording, retention and evidence of identity5.54

5.55 Flight time limitations

5.61to Flight radiotelephone operator licence5.63

5.77to Private pilot (aeroplane) licence5.86

5.103 to Commercial Pilot (Aeroplane) Licence5.119

133Conditions of flight - general134

138(4) Compliance with Flight Manual

146 Liability as to neglect of rules regarding lights, etc.

149 to Flight rules159

160 to Rules of the air181

182 to Signals for the control of Air Traffic196

....




0.4 CARs AND THE FLIGHT CREW MEMBER

215(9)215(10)

Compliance with Operations Manual

219 Route qualifications of pilot in command of a charter aircraft

225 Pilots at controls

232(4) Flight check system to be carried out in detail

233 Responsibility of pilot in command before flight

234(1) Fuel requirements

239 Planning of flight by pilot in command

243 Listening watch

244 Safety precautions before take-off

245 Tests before and during take-off run

247 Meteorological conditions observed enroute

248(1) Reporting defects

253 Competency in emergency procedures

256 Intoxicated persons not to act as pilots

L281 to Penal provisions284

294(3) Authority of pilot in command under the penal provisions

299 Change of address

309 Powers of pilot in command

309A Instructions about activities on board aircraft




0.5 CAOs RELEVANT TO CLUB OPERATIONS

It shall be the responsibility of the pilot in command of the aircraft to know the

requirements of and comply with those Parts or Sections of the following Civil

Aviation orders that are appropriate to the intended operation.

PART 20 Air Service Operations

20.2 Safety precautions before flight

20.3 Marshalling and parking of aircraft

L 20.4 Provision and use of oxygen and protective breathing equipment

20.7.4 Aeroplane weight and performance limitations - Aeroplanes not

above 5700 Kg

20.9 Precautions in refuelling, engine and radar ground operations

20.11 Emergency and lifesaving equipment and requirements for

passenger control in emergencies

20.16 Loading of aircraft

20.17 Use of military aerodromes by civil aircraft

20.18 Aircraft equipment - basic operational requirements

20.22 Taxiing of aircraft by persons other than licensed pilots

PART 29 Miscellaneous

29.5 Dropping of articles from aircraft in flight

PART 40 Pilot Licences and Ratings - Aircraft

40.0 Conditions - Flight crew licences

40.1.0 Aircraft endorsements - aeroplanes

40.2.1 Instrument rating

40.2.2 Night VFR Ratings - Aircraft

40.2.3 Private I.F.R. Rating

....


© AEROSERVICE 2000


0.5 CAOs RELEVANT TO CLUB OPERATIONS

PART 48 Flight Time Limitations

48.0 General

48.1 Pilots

PART 82 Air Operators' Certificates

80.1 Flying school licence

82.0 General requirements

82.1 Conditions on charter and aerial work certificates


© AEROSERVICE 2000


0.6 CONVERSION TABLES

Conversion factors and tables are appended overleaf in the order listed below:

* Standard Conversion Factors

* Celsius - Fahrenheit

* Metres - Feet

* Kilometres - Nautical Miles

* Kilograms - Pounds

* Kilopascals - Pounds sq.inch

* Conversion Diagrams

* Litres - Imperial Gallons

* Litres - US Gallons

* Litres - Kilograms, AVGAS





STANDARD CONVERSION FACTORS Deg.C Deg.F

DISTANCE -60 -76

1 metre = 3.282 feet -50 -58

1 foot = 0.305 metres -40 -40

1 kilometre = 0.54 nautical miles -30 -22

1 nautical mile = 1.854 kilometres -20 - 4

WEIGHT -10 14

1 kilogram = 2.205 pounds 0 32

1 pound = 0.454 kilograms 10 50

VOLUME 20 68

1 US gallon = 0.833 imperial gallon 30 86

1 US gallon = 3.785 litres 40 101

1 imp. gallon = 4.456 litres 50 122

1 imp. gallon = 1.201 US gallon 60 140

1 US quart = 1 litre (approx) 70 158

1 litre = 0.264 US gallon 80 176

1 litre = 0.22 imperial gallon 90 194

TEMPERATURE 100 212

5 x (EF) = 9 x (EC) + 160 110 230

SPECIFIC GRAVITY 120 248

1 litre AVGAS = 0.72 kilograms 130 266

1 imp. gallon AVGAS = 7.2 pounds 140 284

1 litre AVTUR = 0.79 kilograms 150 302

1 imp. gallon AVTUR = 7.9 pounds 160 320

1 litre AVTUR = 1.74 pounds 170 338

PRESSURE 180 356

1 pound sq.in.(psi) = 6.895 kilopascals 190 374

1 kilopascal = 0.145 pounds sq.in. 200 392

L Minutes to Decimal Hours 210 410

Min Dec Min Dec 220 428

0-6 0.1 31-36 0.6 230 446

7-12 0.2 37-42 0.7 240 464

13-18 0.3 43-48 0.8 250 482

19-24 0.4 49-54 0.9 260 500

25-30 0.5 55-60 1.0


© AEROSERVICE 2000



Metres Feet Kms NMs

0.305 1 3.281 1.85 1 0.54

0.610 2 6.562 3.71 2 1.08

0.914 3 9.842 5.56 3 1.62

1.219 4 13.123 7.42 4 2.16

1.524 5 16.404 9.27 5 2.70

1.829 6 19.685 11.12 6 3.24

2.134 7 22.966 12.98 7 3.78

2.438 8 26.247 14.83 8 4.31

2.743 9 29.528 16.69 9 4.85

3.048 10 32.808 18.54 10 5.40

6.096 20 65.616 37.08 20 10.79

7.620 25 82.022 46.35 25 13.48

15.240 50 164.043 92.70 50 26.97

30.480 100 328.086 185.40 100 53.94

370.80 200 107.87

556.20 300 161.81

741.60 400 215.75

927.00 500 269.69


© AEROSERVICE 2000



Kgs Lbs kPa PSI

0.4546 1 2.205 6.90 1 0.15

0.9072 2 4.409 13.79 2 0.29

1.3608 3 6.614 20.69 3 0.44

1.8144 4 8.818 27.58 4 0.58

2.2680 5 11.023 34.48 5 0.73

2.7216 6 13.228 41.37 6 0.87

3.1752 7 15.432 48.27 7 1.02

3.6287 8 17.637 55.16 8 1.16

4.0823 9 19.841 62.06 9 1.31

4.5359 10 22.046 68.95 10 1.45

9.0718 20 44.092 137.90 20 2.90

11.3389 25 55.116 172.38 25 3.63

22.6797 50 110.232 344.75 50 7.25

45.3593 100 220.464 689.50 100 14.50

1379.00 200 29.00

1723.75 250 36.25

2068.50 300 43.50


© AEROSERVICE 2000



Litres Imp. Galls. Litres US Galls

4.55 1 0.22 3.78 1 0.26

9.09 2 0.44 7.57 2 0.53

13.64 3 0.66 11.36 3 0.79

18.18 4 0.88 15.14 4 1.06

22.73 5 1.10 18.93 5 1.32

27.28 6 1.32 22.71 6 1.58

31.82 7 1.54 26.50 7 1.85

36.37 8 1.76 30.28 8 2.11

40.91 9 1.98 34.07 9 2.38

45.46 10 2.20 37.85 10 2.64

90.92 20 4.40 75.71 20 5.28

130.38 30 6.60 94.64 25 6.60

181.84 40 8.80 189.26 50 13.21

227.30 50 11.00 283.90 75 19.81

340.95 75 16.50 378.52 100 26.42

454.60 100 22.00 567.78 150 39.63

1136.50 250 55.00 757.04 200 52.84

2273.00 500 110.00 946.30 250 66.05


© AEROSERVICE 2000



AVGAS - SG 0.72

Litres Kilograms

1.39 1 0.72

2.78 2 1.44

4.17 3 2.16

5.56 4 2.88

6.95 5 3.60

8.34 6 4.32

9.73 7 5.04

11.12 8 5.76

12.50 9 6.48

13.89 10 7.20

27.78 20 14.40

34.73 25 18.00

69.45 50 36.00

104.17 75 54.00

138.89 100 72.00

208.34 150 108.00

277.78 200 144.00

347.23 250 180.00

GG

THIS PAGE INTENTIONALLY LEFT


04/04 THE REDCLIFFE AERO CLUB Section AOPREFACE PAGES Appendix 1

Page 1


ERRATUM/REQUEST FOR CHANGE FORM

Name: Date:

Section/subsection/paragraph:

Page No:

Subject:

For Office Use Only:

Date Received:

Action Taken:

Operations Manual Amended Yes/No Amendment No:

Chief Pilot Signature: Date:


11/05 THE REDCLIFFE AERO CLUB Section AOL PREFACE PAGES Appendix 2

Page 1



11/05 THE REDCLIFFE AERO CLUB Section AOL PREFACE PAGES Appendix 2

Page 2




08/00 OPERATIONS MANUAL A1-1

SECTION A1

GENERAL

SUB-SECTION PAGE

1.1 AIR OPERATORS' CERTIFICATE A1-3

1.2 CAR 215 DIRECTIONS, PERMISSIONS AND APPROVALS A1-3 1.3 OUTLINE OF ORGANISATION STRUCTURE A1-5

1.4 RESPONSIBILITIES OF CLUB PERSONNEL A1-5

1.5 PROCEDURE FOR APPLYING FOR EXEMPTIONSAGAINST CAO 48 A1-9

1.6 AUTHORITY AND RESPONSIBILITIES OF PILOT IN COMMAND A1-9

1.7 CARRIAGE OF FLYING OPERATIONS INSPECTORSOR APPROVED TEST OFFICERS A1-10

1.8 REFUSAL OF PASSENGERS AND/OR CARGO A1-11

1.9 PRECEDENCE OF APPROVED FLIGHT MANUAL A1-13

1.10 USE OF METRIC UNITS OF MEASUREMENT A1-13

1.11 INTERNATIONAL OPERATIONS Reserved

1.12 STAFF RESPONSIBILITY FOR SERVICEABILITYAND ISSUE OF EMERGENCY AND LIFESAVING EQUIPMENT A1-13

1.13 CREW AND STAFF TRAINING IN USE OF EMERGENCYEQUIPMENT A1-14

1.14 DETAILS OF AND STANDARDS FOR AERODROMES A1-14

1.15 PILOT RESPONSIBILITIES IN RESPECT OFUSE OF AERODROMES A1-15

1.16 STANDARD CLUB ROUTES Reserved

1.17 ILLEGAL ACTIVITIES AND CONSEQUENCES A1-17....




SECTION A1

GENERAL

SUB-SECTION PAGE

1.18 AIRCRAFT MAINTENANCE FLIGHTS A1-17

1.19 ALCOHOL AND DRUG USAGE BY CLUB PERSONNEL A1-18

1.20 FLIGHT SAFETY PROGRAM Reserved

1.21 FLYING AFTER DIVING A1-18

1.22 REPORTING OF DEFECTS A1-19

1.23 REFERENCE LIBRARY A1-19

1.24 USE OF GLOBAL POSITIONING SYSTEMAS AID TO IFR NAVIGATION A1-20

APPENDIXES:

1. AIR OPERATORS' CERTIFICATE

2. CAR 215 DIRECTIONS, PERMISSIONS AND APPROVALS

3. NAMES AND CONTACT TELEPHONE NUMBERS

4. CREW MEMBER EMERGENCY PROCEDURES PROFICIENCY TEST ANDCERTIFICATE OF PROFICIENCY

5. ALA REGISTER

L


© AEROSERVICE 2000

08/00 GENERAL A1-3

1.1 AIR OPERATORS' CERTIFICATE

(1) A copy of the Air Operators' Certificate together with any attachments thereto

issued to THE REDCLIFFE AERO CLUB, shall be inserted behind this Section as

Appendix 1 to form part of the Club's Operations Manual.

(2) The Air Operators' Certificate authorises the class of operations and the

aircraft that may be used in those operations and specifies the conditions

under which the certificate is issued.

(3) If the Club intends to enter to an arrangement with another entity for the

operation of aircraft, conduct of an operation or employment of that entity's

employees where that entity is the holder of a cancelled, suspended or varied

AOC or intends to apply for the issue of an AOC, the Club shall obtain written

approval from CASA before entering into such an arrangement.

1.2 CAR 215 DIRECTIONS, PERMISSIONS AND APPROVALS

(1) All operational directions, permissions and approvals that may be issued to

THE REDCLIFFE AERO CLUB in connection with any operation conducted under the

terms of its Air Operators' Certificate shall be recorded below.

(2) An operational specification is a direction given by the Civil Aviation Safety

Authority in order to define, limit or authorise certain specified aspects of the

operation being conducted by THE REDCLIFFE AERO CLUB. The material

comprising an operational specification is directed material and therefore it is

deemed to form an integral part of the Club's Operations Manual and must be

complied with at all relevant times.

(3) The privileges of any exemption and authorisation may only be exercised

when a copy of the relevant document is inserted behind this Section in

Appendix 2, the details are entered in the table on the next pages and the

applicable conditions can be complied with.

(4) IT IS THE RESPONSIBILITY OF THE CHIEF PILOT TO ENSURE THIS

RECORD IN EACH COPY OF THE OPERATIONS MANUAL IS MAINTAINED

IN A CURRENT STATUS.



03/09 GENERAL A1-4

1.2 CAR 215 DIRECTIONS, PERMISSIONS AND APPROVALS

Ref. Details

CAO 29.5 BN/204/0 - Flour Bombing/Flying Competitions

CAR 232 Instrument Number 320/98 - Approval of Flight Check Systems

CAR 5.60 Instrument Number AF/SYN/04/00 - Approval of Aeroguidance

Synthetic Trainer and approval of instrument rating and flight crew

credits.

L CAR 232 Instrument Number CASA EX38/2004 - Exemption From Obtaining

Approval Of Flight Check System



08/07 GENERAL A1-5

1.3 OUTLINE OF ORGANISATION STRUCTURE

FINANCIAL MEMBERS OF THE REDCLIFFE AERO CLUB

Management Committee

L CASACHIEF EXECUTIVE

OFFICER

MAINTENANCE

ORGANISATION

SAFETY OFFICER/S CHIEF PILOTHEAD OF AIRCRAFT

MAINTENANCE

DEPT VOCATIONAL

EDUCATION &TRAINING

L CHIEF FLYING

INSTRUCTORLINE PILOTS

INSTRUCTORS

STUDENT PILOTS

For the Names and contact telephone numbers for key Club personnel, refer to

Appendix 3 this Section.

1.4 RESPONSIBILITIES OF CLUB PERSONNEL

(1) Club

(a) THE REDCLIFFE AERO CLUB as a holder of an Air Operators' Certificate

issued by the CASA is responsible for establishing adequate facilities,

including a reference library of operational documents, instituting suitable

procedures and practices, and the employment of adequate numbers of

suitably qualified personnel to provide safe commercial air services. The

operational office of THE REDCLIFFE AERO CLUB is located at Redcliffe

Airport, Nathan Road, Kippa-ring, Qld.

(b) The Management Committee represents the financial members of the

Club.

(c) The Club and its Chief Pilot shall be jointly responsible to the CASA for

the safety of all commercial operations carried out by the Club.

....



08/07 GENERAL A1-6


L (2) Chief Executive Officer (CEO)

The duties and responsibilities of the Chief Executive Officer include:

(a) ensuring that the Club's flight operations are conducted in compliance

with the Civil Aviation Act, the CARs, the CAOs and the Club's

Operations Manual;

(b) ensuring that the appropriate Air Operator Certificate and schedules

thereto, directions, exemptions, permits and approvals are in place, and

are current for the intended period of operation;

(c) ensuring that aircraft Certificates of Airworthiness, Certificates of

Registration and Insurance Certificate are current;

L (d) ensuring that where there is any change in an appointment or in

information notified or supplied to the CASA in relation to any Certificate,

Approval, Authorisation, Direction or Permit issued to the Company, the

appropriate CASA office is notified of the change;

L (e) ensuring that where there is a planned absence or a change in an

appointment as Chief Pilot or Head of Aircraft Maintenance or the

appointed person cannot fulfil the responsibilities of the position, the

CEO shall;

L (i) at least 14 days prior to a planned absence, submit to the CASA for

approval the name of a suitably qualified person who has accepted

the appointment;

L (ii) in the event of an unplanned absence or resignation, advise CASA

as soon as possible. Arrangements shall be made for the name of

a suitably qualified person who has accepted the appointment to be

submitted to the CASA for approval.

(f) upon written notification from CASA or upon demand from an authorised

person, surrendering any document issued or required to be kept under

the CARs;

(g) ensuring that all insurance cover is placed with reputable underwriters,

and that all risks associated with the business and its operations are

current and adequate in terms of the amounts and range of risks to

which the Club is exposed; ....



08/07 GENERAL A1-7


L (3) Chief Executive Officer (CEO)

L (a) as circumstances dictate, contract suitably approved and qualified

organisations and engineers to carry out scheduled and unscheduled

maintenance, checks and defect rectification on Club aircraft and

emergency equipment used in Club operations, in accordance with the

provisions of the CARs. CASRs and the CAOs;

(b) in liaison with the Club's maintenance organisation, procure spare parts

for Club aircraft with emphasis on quality assurance.

(c) contract suitably approved and qualified organisations to maintain

aircraft support equipment in a serviceable condition;

(d) ensuring that all staff, where appropriate, have the applicable Aviation

Security Identification Cards.

(4) Chief Pilot

The Chief Pilot shall be nominated by the Club and approved by CASA. He

/she shall be responsible to the Civil Aviation Safety Authority for the control

of all flight crew training and operational matters affecting the safety of the

Club's flying operations. The Chief Pilot may delegate to other members of the

Club certain duties, but the Chief Pilot ultimately remains responsible to the

CASA for ensuring such duties have been carried out. The Chief Pilot is

responsible for;

(a) ensuring that the Club's air operations are conducted in compliance with

the Civil Aviation Act, the CARs, the CAOs, the AIP and the Club

Operations Manual;

(b) arranging flight crew rosters;

(c) maintaining a record of licences and ratings held by each flight crew

member including validity, recency, type endorsements and any

applicable licence restrictions. Checking of pilots operational documents,

records and log books

(d) maintaining a system to record flight and duty times to ensure

compliance with duty and flight time limitations, in accordance with

sub-section 2.8 of Section A2;

....



08/07 GENERAL A1-8


(3) Chief Pilot (Cont’d)

(e) ensuring compliance with loading procedures specified for the Club

aeroplanes and proper compilation of loading documents including

passenger and cargo manifests;

(f) monitoring operational standards, maintaining training records and

supervising the training and checking of the Club flight crew;

(g) conducting flight crew emergency procedures training and proficiency

tests in accordance with sub-section 1.13, this Section;

(h) supervising the training of Club flight crew by person approved under

CASR 92.140 in the acceptance and/or handling of dangerous goods as

required by sub-section 8.2 of Section A8;

(i) maintaining a complete and up to date reference library of operational

documents as listed in sub-section 1.23, this Section;

(j) overall responsibility for the efficient operation of the Club's aeroplanes;

(k) the production and amendment of the Club's Operations Manual, and

any variation thereof and to liaise with the Civil Aviation Safety Authority

regarding this Manual;

(l) ensuring that every flight is strictly in accordance with the terms,

conditions and limitations of the Club's aviation insurance policies;

(m) the exercise of disciplinary authority over all flight crew personnel;

(n) maintaining records of each and every test required by the current CAOs

and the Club's conclusions based on each such test and practice as to

the relevant person's competence to perform his/her required flight crew

duties. These records are to be kept for minimum of two years.

(5) Chief Flying Instructor

Refer to Part E

....



08/07 GENERAL A1-8a


L (6) Head of Aircraft Airworthiness and Maintenance Control (HAAMC)

The HAAMC shall be nominated by the Club and approved by CASA. He/sheis responsible for controlling the airworthiness and maintenance of Companyaircraft and ensuring that the following are properly carried out including, butnot limited to;

(a) The monitoring of aircraft hours, cycles and other information relevantto the scheduling of maintenance;

(b) The scheduling of maintenance;

(c) The monitoring and scheduling of maintenance due, and deferredmaintenance actions (including deferred defects);

(d) Compliance with Airworthiness Directives in accordance with sub-section3.10(4);

(e) Arrangement of defect rectification and unscheduled maintenance;

(f) The investigation and reporting of defects in accordance withsub-section 3.10(5);

(g) Monitoring the continued effectiveness of the aircraft’s maintenanceprogram;

(h) The monitoring and assessment of aircraft trend monitoring (ifapplicable);

(i) The monitoring of weight control, scheduling of aircraft weighing anddistribution of weight and balance data in accordance with sub-section3.10(9);

(j) Engaging and monitoring the performance of the nominatedmaintenance provider in accordance with sub-section 3.10(13);

(k) The maintenance and security of aircraft and aircraft component records;

(l) Control and storage of Club purchased aircraft components inaccordance with sub-section 3.14;

(m) Liaising with CASA;

(n) maintaining a program showing the following information;

(i) aircraft schedule maintenance and special inspections;

(ii) aircraft hours and cycles;

(iii) emergency, ground support and role equipment maintenanceschedule.

....



08/07 GENERAL A1-8b


(7) Line Pilots

When rostered to fly as pilot in command of Club aeroplane, the pilot

concerned is responsible for the proper disposition of the aeroplane at all

times, including;

(a) Observance of the applicable requirements and procedures in the Club's

Operations Manual;

(b) Ensuring that each flight is conducted in accordance with any rule,

regulation or condition prescribed for that flight;

(c) Compliance with all relevant Commonwealth and State laws, regulations

and directions;

(d) Carryout the necessary functions during an emergency or during an

emergency evacuation as detailed in sub-section 5.10(2) of Section A5;

(e) Completion of all records required to be completed in respect of that flight;

(f) Safety of the aeroplane and all persons and cargo carried during flight

time;

(g) Complying with any demand by an authorised person to produce

licences, log books, certificates, aircraft documentation, passenger list

or manifest for inspection.

INTENTIONALLY LEFT BLANK


© AEROSERVICE 2000

08/00 GENERAL A1-9

1.5 PROCEDURE FOR APPLYING FOR EXEMPTIONS AGAINST CAO 48

(1) The Civil Aviation Safety Authority will consider applications for particularflights and reduced rest periods. The applications for exemptions, setting outall the relevant particulars as specified in CAO 48.0, paragraph 4.1, shall bemade by the Chief Pilot in writing to the appropriate office of the Civil AviationSafety Authority for consideration.

(2) The details of any exemptions granted must be recorded at sub-section 1.2and a copy of the exemptions inserted in Appendix 2 to this Section beforesuch privileges may be exercised.

1.6 AUTHORITY AND RESPONSIBILITIES OF PILOT IN COMMAND

(1) For each flight the Club shall nominate on the Club's roster the pilot incommand and the pilot so nominated carries full responsibility for the safe andefficient conduct of the flight to its ultimate completion, or until handing overthe aircraft at a point where a crew change takes place. If two pilots arerostered to act as flight crew together, the more senior pilot shall benominated as the pilot in command.

(2) By virtue of CAR 224 and 309, the Club authorises the pilot in command asthe final authority when exercising operational control of the aeroplane.

(3) A Club pilot may act as pilot in command under supervision for the purposeof gaining experience on a particular aeroplane type or experience for aparticular type of operation provided;

(a) the pilot acting as pilot in command under supervision shall be the co-pilot of the aeroplane and shall hold at least a commercial pilot(aeroplane) licence, an endorsement on the aeroplane type in use andshall hold, if required for the conduct of the flight, the applicable ratingfor the intended operation, that permits him/her to fly as pilot incommand; and

(b) a Club Instructor, who holds at least a Grade 3 flight instructor rating,conducts the supervision and he/she holds an endorsement on theaeroplane type in use that allows that instructor to act as pilot incommand and, if required, the applicable rating for the intendedoperation that permits him/her to fly as pilot in command; and

(c) the pilots referred to in (a) and (b) above shall be approved by the ChiefPilot for the purpose.



04/04 GENERAL A1-10

1.7 CARRIAGE OF FLYING OPERATIONS INSPECTORS OR APPROVED TEST

OFFICERS

(1) From time to time a CASA Flying Operations Inspector (FOI) or an Approved

Test Officers (ATO) may be authorised to undertake an inspection or check

of Club procedures or of the operation of a particular aircraft or item of

equipment. Flights of this nature will be co-ordinated through the Chief Pilot

and normal courtesies will be extended to that Officer whilst flying with the

Club.

(2) Where a flight test is to be conducted in a Club aeroplane on which the FOI

or ATO conducting the flight test is qualified to act a pilot in command, the

FOI or ATO shall be designated as pilot in command for that flight.

(3) Where the applicant to be given a flight test is otherwise qualified to act as

pilot in command on the aeroplane type and the FOI or ATO is not qualified

to act as pilot in command on the aeroplane type, then the applicant shall be

designated as the pilot in command for that flight.

(4) Before an FOI or ATO acts as pilot in command of a Club aeroplane, the FOI

or ATO shall meet the Club minimum requirements detailed in sub-section 2.6

for a pilot in command and that formalities, e.g. familiarisation with Club

Operations Manual, are completed.

L (5) The pilot in command of the aircraft retains the right to ask a CASA officer to

produce proof of identity and/or authorisation prior to any such carriage. If

proof of identity and/or authorisation is not produced by the CASA Officer, the

pilot in command shall immediately contact the Chief Pilot who shall refer the

matter to the applicable CASA office.



© AEROSERVICE 2000

08/00 GENERAL A1-11

1.8 REFUSAL OF PASSENGERS AND/OR CARGO

(1) General

(a) Under the provisions of CAR 309 and with the full authority and approvalof the Club, the pilot in command may refuse the carriage of persons andof any goods or other substances if, in the pilot's opinion, a breach of CivilAviation Regulations will be or is likely to be made.

(b) No passenger shall be carried on board a Club aeroplane while thataeroplane is;

(i) conducting a maintenance flight; or

(ii) a flight for the purpose of;

- endorsing a pilot on that aeroplane;

- practice of emergency procedures;

- low flying practice or

- aerial work operations.

(2) Passengers

Authority is vested in the pilot in command to refuse embarkation to, or orderthe disembarkation of, any person whose behaviour is or is potentially withinthe following categories:

(a) Apparently intoxicated or under the influence of drugs to the extent ofphysical incompetence such as inability to safely board the aircraft or toobserve various ramp/aircraft safety or emergency instructions.

(b) Disorderly or offensive conduct which causes or may cause discomfortor distress to other passengers and/or crew.

(c) Violent to the extent of possible damage to, or hazard to the safety of,the aircraft.

(d) Apparently of unsound mind.

(e) Known or suspected to be in possession of an unauthorised firearm orother weapon.

(f) Not observing the reasonable instructions of ground staff to comply witha safety requirement stipulated by the Civil Aviation Regulations.

....



04/04 GENERAL A1-12


L (3) Crew and Passenger Baggage Restrictions

Articles and substances which are classified as dangerous goods must not be

carried in baggage intended to be carried in a baggage compartment, as carry-

on baggage or on their person except as permitted in sub-section 8.3(1)(a)

of Section A8.

(4) Firearms

(a) A firearm will only be accepted for carriage on a Club aeroplane

engaged aerial work operations in accordance with the following;

L (i) the Club is in possession of a permit granted by the CASA for the

carriage of firearms on Club aeroplanes; and

(ii) the firearm must be empty of ammunition; and

(iii) where the bolt cannot be removed from the firearm, the firearm shall

be carried on that aeroplane in a baggage compartment that is not

accessible from the cabin while the aeroplane is in flight, or

(iv) where the bolt can be removed from the firearm, the firearm may be

carried in the cabin of the aeroplane provided the bolt is removed

and carried in a baggage compartment that is not accessible from

the cabin while the aeroplane is in flight; or

(v) the firearm may be carried in the cabin of the aeroplane in which no

persons, other than the pilot, is on board.

(b) Persons, including police or security officers who are required to carry

firearms in the course of duty, are not permitted to carry firearms in the

passenger compartment of a charter aircraft except where the person

has written permission from the Department of Transport and

Communications under Section 22D(2)(a) of the Air Navigation Act for

the carriage of such firearms. The Club shall ensure that firearms are

only carried in accordance with the conditions of the applicable permits

granted. Such written permission does not negate the right of the Club

or the pilot in command to refuse the carriage of the firearms.

....



04/04 GENERAL A1-13


(5) Cargo

L (a) Club personnel are cautioned that certain articles which may be requiredfor carriage on board Club aeroplanes could be hazardous. Any articleswhich are found to contain dangerous goods, except as permitted insub-section 8.3(1) of Section A8, cannot be accepted for carriage in Cluboperated aeroplanes;

L (b) For the guidance of all operational personnel, a list of possiblehazardous articles is contained in Appendix 3 to Section A8.

1.9 PRECEDENCE OF APPROVED FLIGHT MANUAL

(1) The pilot in command shall comply with all the requirements, procedures,limitations and material specifications applicable to the operation of theaircraft as specified in the Flight Manual for that aircraft.

(2) Where the aeroplane's Flight Manual conflicts with the manufacturer'sinformation or any other published data, the Flight Manual shall take precedence.

1.10 USE OF METRIC UNITS OF MEASUREMENT

Metric units of measurement shall be used wherever practicable, but thisnotwithstanding, Flight Manual data may be expressed in units of measurementsconsistent with the markings and placards of the particular aircraft.

NOTE: See conversion factors at sub-section 0.6 of Section AO, this Part.

1.12 STAFF RESPONSIBILITY FOR SERVICEABILITY AND ISSUE OF EMERGENCYAND LIFESAVING EQUIPMENT

(1) The pilot in command is responsible for ensuring that emergency andlifesaving equipment is carried on those flights on which the CARs or theCAOs stipulate emergency and lifesaving equipment shall be carried and thatsuch equipment conforms to the standards in the CAO applicable to theparticular equipment. The requirements applicable to this Club are specifiedin sub-section 6.30 of Section A6, sub-sections 5.6, 5.7 and 5.8 of Section B5,Part B and sub-section 0.9(3) of Section DO, Part D..

(2) Prior to commencing any such flight, the Club and the pilot in command mustensure that each item of emergency and lifesaving equipment aboard theaircraft aeroplane is not "time expired" and is in such condition that it willsatisfactorily perform its designated function.

(3) The pilot in command will ensure life jackets and/or life rafts, when required,are stowed in such a manner that they are immediately accessible by alloccupants.



04/04 GENERAL A1-14

1.13 CREW AND STAFF TRAINING IN USE OF EMERGENCY EQUIPMENT

(1) The Chief Pilot shall ensure that a person does not act as crew member of aClub aeroplane unless he/she has undertaken and passed the proficiency testin emergency procedures specified in Appendix IV of CAO 20.11 on that typeof aeroplane.

L (2) Such tests, conducted by the Chief Pilot, shall be taken and passed annuallyand upon satisfactory completion, a Certificate of Proficiency for that aircrafttype shall be issued by the Chief Pilot and retained in Club records. Theannual test of the Chief Pilot shall be conducted by a CASA FOI or a personapproved by CASA for the purpose.

(3) The form used to record the results of the proficiency test and relevantCertificate of Proficiency is shown at Appendix 4 to this Section.

1.14 DETAILS OF AND STANDARDS FOR AERODROMES

(1) Before electing to use any area for take-off or landing, the pilot in commandshall take all reasonable steps to ensure that the area meets therecommended minimum physical characteristics as specified in Civil AviationAdvisory Publication 92-1(1) for the intended operation and having regard toall the circumstances of the proposed landing or take-off, including the prevailingweather conditions, the aircraft can land or take-off in safety.

(2) Club pilots shall obtain information for government, military or licensedaerodromes from the ERSA and AVFAX NOTAMS to determine if anaerodrome is suitable Club operations.

(3) For other than aerodromes referred to in (2) above, the Club's AeroplaneLanding Area (ALA) Register records details of the landing areas which arein regular use by the Club. If an area is not listed in the ALA Register, the pilotshall obtain the required information, as detailed in the ALA description form,from the owner or operator of the facility, to confirm that the area meets theminimum requirements as required by (1) above, before using that area. Theinformation obtained shall be entered into the Club's ALA Register, asapplicable.

(4) No aerodrome landing area may be used without the prior consent of theowner, occupier or controlling authority of that place but, in some cases, suchconsent may be in the form of a 'blanket approval' which shall be noted on theapplicable ALA Register.

....


© AEROSERVICE 2000

08/00 GENERAL A1-15

1.14 DETAILS OF AND STANDARDS FOR AERODROMES

(5) Page 1 of Appendix 5 to this Section shows a copy of the Club's AeroplaneLanding Area Description. The Appendix makes provision for the Club'sregister of ALAs to be inserted behind the Index page. Each ALA descriptionshall be recorded numerically in the index of the ALA Register and a copyinserted behind that Register page.

(6) It is the responsibility of the Chief Pilot to ensure the ALA Register is maintainedin a current status. He/she shall review and verify the accuracy of the informationon each ALA listed in the ALA Register on a bi-annual basis. The date of thelast review shall be recorded on the particular ALA description form.

1.15 PILOT RESPONSIBILITIES IN THE USE OF AERODROMES

(1) Club pilots may use the data published in the ERSA or the Club's ALA registerfor determining if an area is suitable for operations in Club aeroplanes inaccordance with the following;

(a) after checking NOTAM information for information that may preclude orrestrict operations at the area of intended operation;

(b) if the area is unlicensed, after contacting the owner or operator to obtain orconfirm the information required by the ALA description form.

(2) Before electing to use an area as a landing area, the pilot in command shalltake all reasonable steps to ensure that:

(a) the landing area meets the physical characteristics or has obtainedapproval as required by sub-section 1.14(1) above;

(b) hazardous obstacles or obstructions are noted;

(c) for the intended operation, having regard to all the circumstances of theproposed landing or take-off including the prevailing weather conditions,the aeroplane can land or take-off in safety;

(d) the characteristics of the aeroplane and the operating technique employedwill permit safe operations under the ambient meteorological conditions;

(e) the limitations of any area affected by Federal, State or Local Councillegislation covering noise or other environmental considerations areobserved; and

(f) the surface strength and condition, including height of grass and othervegetation, will permit safe landing and take-off.

....


© AEROSERVICE 2000

08/00 GENERAL A1-16

1.15 PILOT RESPONSIBILITIES IN THE USE OF AERODROMES

(3) Adequate precautions shall be taken by the pilot to ensure that objects,

animals and persons not essential to the immediate operation are clear of the

total area of the ALA during approach and take-off operations. In any event,

the pilot shall not approach, take-off or manoeuvre the aeroplane within 30

metres of animals or persons not essential to the immediate operation.

(4) When operating to or from a military aerodrome other than a joint civil/military

aerodrome the pilot in command shall apply for authorisation for the intended

operation to the relevant military authority and he/she shall ensure that the

requirements of any authorisation granted are complied with while operating

at the particular military aerodrome.

(5) Should a pilot observe any defect or hazardous condition at a landing area

listed in the Club's ALA Register or other document, he/she shall report the

matter to the owner/occupier of that place and advise the Chief Pilot who will

ensure the particular ALA Register, if applicable, is annotated accordingly and

then liaise with the owner/occupier to have that condition rectified.

WARNING

The fact that permission may have been granted for a particular place to be

used as a landing area does not confer any right on this Club or the pilot in

command to alight on or take-off from that area as against the owner of the

land or any person interested therein, or prejudice the rights or remedies of

any person in respect of any injury to persons or property resulting from the

use of that area.

(6) If for any reason a Club aeroplane is left on the movement area of an

aerodrome, in an area which is not designated for the parking of aeroplanes

or in an area so as to constitute a hazard to aircraft operations, the pilot in

command shall ensure that the details of the position of the aeroplane and the

hazard is reported to ATS as soon as practicable.



06/02 GENERAL A1-17

1.17 ILLEGAL ACTIVITIES AND CONSEQUENCES

L (1) Section 20A of the Civil Aviation Act stipulates that a person must not operatean aircraft in a reckless manner which could endanger life or could endangerthe person or property of another person..

(2) In any event, a pilot who flies, or any person who acts in contravention of aprovision of the Civil Aviation Act or the Civil Aviation Regulations or a personwho hinders or obstructs any person performing a duty under the CARs isguilty of an offence and, in addition to any action which the Club may take,could be fined or prosecuted by the CASA depending on the circumstancesand nature of the offence.

(3) Club staff shall not supply misleading information for, or falsify, any Clubdocumentation, personal documentation or an application for the issue,renewal or endorsement of a licence, rating, certificate, permit, permission,authority or approval in relation to qualifications or experience.

(4) Where a Club pilot has had a licence, certificate or a rating or endorsementon a licence cancelled or suspended, that pilot shall notify the Chief Pilotimmediately and shall not exercise the privileges of that licence, certificate,rating or endorsement during the period of cancellation or suspension.

1.18 AIRCRAFT MAINTENANCE FLIGHTS

(1) Flights, for maintenance purposes, shall only be carried out by the Chief Pilot,or a pilot specifically authorised by the Chief Pilot for that purpose.

L (2) Any aircraft proceeding on a test flight shall carry its normal flight crewcomplement and, if required for the purpose of the flight, maintenancepersonnel, and shall possess a current Maintenance Release or Special FlightPermit, as applicable.

(3) Maintenance flights shall be conducted automatically for any one of thefollowing reasons:

(a) After major overhaul or rebuild.

(b) After any primary control has been changed.

(c) After engine change.

(d) At the request of the Club's maintenance organisation.



03/09 GENERAL A1-18

1.19 ALCOHOL AND DRUG USAGE BY CLUB PERSONNEL

(1) A Club pilot shall not act as a member of the operating crew of a Club aircraftor perform any preparatory duties or functions, if he/she has consumedalcoholic liquor during the period of eight hours immediately before thedeparture of the aircraft.

(2) Flight crew members shall not consume any alcoholic liquor during their tourof duty or reserve time, as applicable.

(3) A pilot shall not act as a member of the operating crew of an aircraft orperform any of the associated duties or functions if his/her capacity to so actis, or is likely to be, impaired as a result of having consumed, used, orabsorbed any alcoholic liquor, drug, pharmaceutical or medicinal preparationor other substance.

(4) Should the use of prescribed drugs by pilots raise the question of licencevalidity, the opinion of a CASA approved medical examiner must be obtained.

L (5) Refer to the Club’s Drug and Alcohol Management Plan for the Club’s policy andprocedures in relation to alcohol and other drug use that may affect the healthand safety of Club employees, contractors, sub-contractors and passengers.

1.21 FLYING AFTER DIVING

(1) Where a pilot or a passenger is involved in underwater diving activities, thatperson should be aware of the problems and limitations associated with flyingafter diving.

NOTE: 'Snorkelling' does not constitute underwater diving.

(2) The problem which may occur by flying after diving is decompression sickness(bends). This is a condition which may occur with divers if they have spent a longperiod of time at depth and return to the surface too quickly. It is a function of thedepth of the dive, time spent at depth and speed of return to the surface. If aperson is subjected to a further reduction of atmospheric pressure (e.g. flying),there is a higher probability of developing decompression sickness.

(3) The following are the recommended limitations for flying after diving:

(a) Diving which does not require decompression stops may be followed byflying after a rest at sea level of 4 hours;

(b) Diving which requires decompression stops and is of less than 4 hoursduration may be followed by flying after a sea level rest of 12 hours;

(c) Diving which requires decompression stops and is of more than 4 hoursduration may be followed by flying after a sea level rest of 48 hours.



03/09 GENERAL A1-19

1.22 REPORTING OF DEFECTS

(1) All defects in a Club aeroplane or a aeroplane component shall be entered on

the current Maintenance Release and reported to the Chief Pilot and, where

applicable, the owner of the aeroplane. If the defect is in the aeroplane, a

component or in a maintenance procedure and use of the aeroplane, the

installation of that component or the use of that procedure might have affected

the safety of the aeroplane, the Chief Pilot or, where applicable the owner of

the aeroplane, shall have the defect investigated and reported in accordance

with sub-section 3.10(5) of Section A3.

(2) The method of recording unserviceabilites is described in sub-section 3.1 and

3.2 of Section A3, this Part.

(3) Defects observed in air routes, aerodromes, air route facilities or airways

facilities shall be reported to the appropriate Authority.

1.23 REFERENCE LIBRARY

L (1) The Club shall establish and maintain a Reference Library at the Club’s office

for use by operational personnel. The library shall consist of the following

documents and shall be held in the locations as detailed below.

L (2) Operations Office

(a) Club Operations Manual;

(b) Civil Aviation Act;

(c) Civil Aviation Regulations;

(d) Civil Aviation Orders, (Parts, 20, 40, 48, 82, 92, 95, 100);

L (e) Transport Safety Investigation Act 2003 and associated Regulations;

L (f) Aviation Transport Security Act 2004 and associated Regulations;

(g) Aeronautical Information Publication and AIP supplements;

(h) DAP East and West;

(i) Aeronautical Information Circulars as issued to AIP holders;

(j) Civil Aviation Advisory Publications;

(k) Aeroplane Landing Area register;

(l) Airworthiness Advisory Circulars;

L (m) Drug and Alcohol Management Plan;

(n) World Aeronautical Charts and Radio Navigational Charts appropriate

to the area of operation.

....



03/09 GENERAL A1-20

1.23 REFERENCE LIBRARY

L (3) Aircraft

(a) Aircraft Flight Manuals for the aircraft the Club is presently operating.

These documents shall be located in the respective aircraft;

(b) Pilot Operating Handbook for each aircraft type the Club is presently

operating. These documents shall be located in the respective aircraft.

L (4) The Club may, at the discretion of the Chief Pilot, use the CASA web site or

the latest edition of the CASA Document Library CD-ROM in lieu of the paper

version of the equivalent documents referred to in (2) above. The computer

used to access these documents shall be readily available to operational

personnel.

(5) Revisions

(a) The Chief Pilot will ensure that revisions to the “hard copy” documents

listed in (1) above are inserted as soon as possible after receipt, or if an

effective date is published, on that date. Details of the revisions shall be

entered in the revision record for the applicable document. Any

notifications of insertion of amendments shall be completed and returned

to the issuing authority.

(b) The Chief Pilot shall download, from the CASA web site, amendments

issued to the contents of the CASA Document Library CD-ROM on a

weekly basis. These amendments shall be made available to all

operational staff.

(6) Responsibility

(a) The Chief Pilot shall that ensure that an amendment service in place

with each issuing authority or manufacturer to maintain current and up

to date documents at all times.

(b) Club personnel are required to have a working knowledge of the contents

of the library and the Club shall ensure that the library is accessible to Club

personnel while performing their assigned duties.



06/02 GENERAL A1-21

1.24 USE OF GLOBAL POSITIONING SYSTEM AS AN AID TO IFR NAVIGATION

(1) General

This sub-section details the requirements for the use by Club pilots of GlobalPositioning System (GPS) as an en route and area IFR primary meansnavigation aid and a navigation aid for the purpose of "GPS Arrivals", "DMEor GPS Arrivals" and "GPS/NPA" as published in AIP DAP/Jeppesen AirwayManual.

(2) Definitions

SOLE MEANS NAVIGATION SYSTEM; A navigation system that, for a given phaseof flight, must allow the aircraft to meet all four navigation system performancerequirements - accuracy, integrity, availability and continuity of service.

PRIMARY MEANS NAVIGATION SYSTEM; A navigation system that, for a givenoperation or phase of flight, must meet accuracy and integrity requirements, butneed not meet full availability and continuity of service requirements, Safetyis achieved by either limiting flights to specific time periods, or throughappropriate procedural restrictions and operational requirements.

SUPPLEMENTAL MEANS NAVIGATION SYSTEM; A navigation system that must beused in conjunction with a sole means navigation system.

INTEGRITY; That quality which relates to the trust which can be placed in thecorrectness of information supplied by a system. It includes the ability of asystem to provide timely warnings to users when the system should not beused for navigation.

RECEIVER AUTONOMOUS INTEGRITY MONITORING (RAIM); A technique wherebyan airborne GPS receiver/processor autonomously monitors the integrity ofthe navigation signals from GPS satellites.

NOTE: Systems for providing integrity, other than RAIM, may be approved foruse, Where reference to RAIM occurs in this sub-section, it includesother approved equivalent integrity monitoring systems.

Prior knowledge of RAIM availability will enable operators and pilots to use thesystem more efficiently, by allowing operations to be planned around gaps inRAIM coverage. Flights should be planned to ensure the safe completion offlight in the event of loss of GPS integrity. Pilots should request a GPS statusreport from NAIPS or access the RAIM prediction page of the GPS equipmentto establish RAIM availability for the proposed flight.



06/02 GENERAL A1-22


(3) Limitations

Club pilots may use a GPS system, fitted and operated in accordance with the

provisions of this sub-section, within Australian domestic airspace only, for the

purpose of:

(a) position fixing, as required in the AIP;

(b) long range navigation in accordance with AIP, including operations on

designated RNAV routes;

(c) deriving distance information, for en route navigation. traffic information

and ATC separation;

(d) en route IFR descent below LSALT/MSA - GPS Arrivals;

(e) en route IFR descent below LSALT/MSA - DME or GPS Arrivals

(substituting GPS derived distance information); and

(f) application of RNAV based separation.

(g) use as an en route supplemental navigation aid;

(h) GPS Non Precision Approaches (GPS NPA).

(4) Airworthiness Requirements

Before GPS equipment may be used for IFR operations in Club aeroplanes,

the following airworthiness requirements must be satisfied:

(a) GPS navigation equipment must have US FAA Technical Standard

Order TSO C-129 (or CASA approved equivalent) authorisation; and

(b) GPS receivers must be installed in accordance with the AAC No 6-26;

and

(c) Automatic barometric aiding function, as provided by TSO C-129, must

be connected.

....



06/02 GENERAL A1-23


(5) Pilot Training

Prior to using GPS in IFR operations for any of the purposes specified in thissub-section, Club pilots must, unless exempted by CASA;

(a) be the holder of an appropriate instrument rating;

(b) have completed a course of ground training and, for GPS/NPA, flighttraining, based on the syllabus contained in Appendix IV to CAO 40.2.1and demonstration of competence in the operation of GPS equipment.The training must be conducted in accordance with sub-section 13.7 ofCAO 40.2.1;

(c) receive instruction by the Chief Pilot in the use of the particular type ofGPS equipment fitted to Club aeroplanes, other than the type ofequipment referred to in (b) above, to ensure that they are familiar withand competent in the operating procedures required for that type ofequipment.

(d) before conducting a GPS/NPA approach in IMC, have completed threeGPS/NPA approaches utilising the same type of GPS receiver.

Satisfactory completion of the training and demonstration of competence inthe operation of GPS equipment must be certified in the pilot's personal logbook by either a Flying Operations Inspector (FOI), or by the person approvedto conduct such training.

(6) Operational Requirements

Before using GPS equipment fitted to a Club operated aeroplane, Club pilotsshall ensure that;

(a) operating instructions for GPS navigation equipment are carried onboard; and

(b) the GPS navigation equipment is operated in accordance with theoperating instructions, and any additional requirements specified in theapproved aircraft Flight Manual or Flight Manual supplement.

(c) In addition to GPS, the aeroplane is equipped with serviceable radionavigation systems as specified at sub-section 1.5(2)(b), Section B1,Part B.

....



06/02 GENERAL A1-24


(6) Operational Requirements

Before using GPS equipment ... (Cont’d);

(d) GPS is not used to satisfy any of the alternate requirements of the AIP.

(e) When within rated coverage of ground based navigation aids, the pilotmust, except when conducting a GPS/NPA, monitor the ground basedsystem and maintain track as defined by the most accurate groundbased radio navigation aid (VOR or NDB) available.

(f) when required by ATC for the application of separation, a GPS equippedaeroplane is to establish on, and track with reference to a particular VORradial or NDB track.

(g) GPS is not used as a navigation reference for flight below theLSALT/MSA, except as provided in 1.24(9) or 1.24(10) below or asotherwise authorised by CASA.

(7) Operations Without RAIM

GPS/NPAs are not approved without RAIM. GPS systems normally providethree modes of operation:

- Navigation Solution with RAIM;

- 2D or 3D Navigation Solution without RAIM; and

- Dead Reckoning (DR), or Loss of Navigation Solution.

When RAIM is lost, the following procedures must be adopted:

(a) Aircraft tracking must be closely monitored against other onboardsystems.

(b) in controlled airspace, pilots must advise ATC if:

(i) RAIM is lost for periods greater than ten minutes, even if the GPSis still providing positional information; or

(ii) RAIM is not available when ATC requests a GPS distance, or if anATC clearance or requirement based on GPS distance is imposed;or

(iii) the GPS receiver is in DR mode, or experiences loss of navigationfunction, for more than one minute; or

(iv) Indicated displacement from track centreline is found to exceed

2NM. ....



06/02 GENERAL A1-25


(7) Operations Without RAIM (Cont’d)

(c) If valid position information is lost (2D and DR Mode), or non-RAIMoperation exceeds ten minutes, the GPS information is to be consideredunreliable, and pilots shall use another means of navigation until RAIMis restored and the aircraft is re-established on track.

(d) Following re-establishment of RAIM, the pilot shall notify the appropriateATS unit of RAIM restoration, prior to using GPS information.

(e) When advising ATS of the status of GPS, the phrases "RAIM FAILURE'or "RAIM RESTORED" must be used.

(8) GPS Distance Information to ATS Units

When a DME distance is requested by an ATS unit, DME derived distanceinformation should normally be provided. Alternatively, GPS derived distanceinformation may be provided to an ATS unit, unless RAIM is currentlyunavailable and has been unavailable for the preceding ten minutes.

Notwithstanding the above paragraph, if an ATC unit has issued a clearanceor requirement based upon GPS distance (e.g. a requirement to reach acertain level by a GPS distance), the pilot shall inform ATC if RAIM is notavailable.

When a DME distance is not specifically requested, or when the provision ofa DME distance is not possible, distance information based on GPS derivedinformation may be provided. When providing GPS distance, transmission ofdistance information must include the source and point of reference - 115 GPSCAIRNS VOR; 80 GPS COEN NDB; 267 GPS VILOK.

If a GPS distance is provided to an ATC unit, and RAIM is not currentlyavailable, but has been available in the preceding 10 minutes, the distancereport should given as "26 GPS COEN NEGATIVE RAIM."

Distance information must only be provided in relation to published waypointsunless specifically requested by an ATS unit.

Where GPS distance is requested or provided from an NDB, VOR, DME, orpublished waypoint, the position of the navigation aid or waypoint must bederived from a vendor supplied database.

....



06/02 GENERAL A1-26


(9) GPS Arrivals

Provided that primary azimuth guidance is provided by an associated NDB orVOR, and subject to the restrictions in the following paragraph, Club pilots,who have completed the appropriate training may use a GPS systems whichmeet the requirements of this sub-section to conduct enroute IFR descentbelow LSALT/MSA in accordance with the "GPS Arrival" or "DME or GPSArrival" procedures published in AIP DAP/Jeppesen Airway Manual.

In addition to the general limitations and restrictions in this sub-section, thefollowing specific restrictions apply to "GPS Arrivals" and "DME or GPSArrivals":

(a) The coordinates of the destination VOR or NDB, to which the descentprocedure relates, must be obtained from a vendor supplied database.

(b) The database medium (card, chip, etc) must be current, and of a kindendorsed by the receiver manufacturer.

(c) RAIM must be available before descending below the LSALT/MSA whenconducting a "GPS Arrival" or "DME or GPS Arrival".

(d) The destination aid (VOR or NDB) nominated in the "GPS Arrival" or"DME or GPS Arrival" chart must be used to provide primary trackguidance during the arrival procedure.

(e) In the event of a significant disparity between the NDB or VOR track,and the GPS track indication, the pilot must discontinue the arrivalprocedure.

(f) If at any time during the approach there is cause to doubt the validity ofthe GPS information (eg, RAIM warning), or if RAIM is lost, the pilotmust:

(i) maintain flight to the Missed Approach Point (MAPT) at the lastlevel at which the pilot was satisfied with the accuracy of the GPSsystem; or

(ii) climb to the en route LSALT/MSA, and use an alternative approach,or hold or divert.

....



06/02 GENERAL A1-27


(10) GPS Non Precision Approaches (GPS/NPA)

Club pilots, who have completed the appropriate training may use a GPS

systems which meet the requirements of this sub-section to conduct

GPS/NPAs in accordance with the GPS/NPA procedures published in AIP

DAP/Jeppesen Airway Manual.

In addition to the general limitations and restrictions in this sub-section, the

following specific restrictions apply to "GPS/NPAs":

(a) the pilot conducting the approach shall;

(i) hold a current instrument rating endorsed with GPS/NPA;

(ii) have completed one GPS/NPA within the past 90 days;

(iii) have completed one GPS/NPA within the past 6 months using the

same type of GPS equipment;

(iv) have completed at least 3 approaches using the same type of GPS

equipment before conducting a GPS/NPA in IMC as pilot in

command;

(b) The coordinates of the waypoints used to construct the approach must

be derived from a vendor supplied database;

(c) Except in an emergency, the database medium (card, chip, etc) must be

current, and of a kind endorsed by the receiver manufacturer;

(d) RAIM must be available for the period during which the approach will be

conducted;

(e) If at any time during the approach there is cause to doubt the validity of

the GPS information (eg, RAIM warning), or if RAIM is lost, the pilot must

immediately commence a missed approach.

(f) An alternate approach based on a conventional navigation aid must be

planned. This approach may be available at the destination aerodrome.

....



06/02 GENERAL A1-28


(11) Data Integrity

Club pilots shall, where possible, derive enroute navigation aid and waypoint

latitude and longitude data from a validated data base, which cannot be

modified by the operator or crew.

Club pilots shall only use data from a validated database for navigation below

the LSALT/MSA. Manually entered data must not be used for navigation by

Club pilots below the LSALT/MSA.

When data is entered manually, data entries must be cross-checked by an

independent check (eg, GPS computed tracks and distances against current

chart data).

Both manually entered and database derived position and tracking information

should be checked for reasonableness in the following cases:

(a) prior to each compulsory reporting point;

(b) at or prior to arrival at each enroute waypoint;

(c) at hourly intervals during area type operations when operating off

established routes; and

(d) after insertion of new data - eg, creation of new flight plan.

(12) Flight Plan Notification

Pilots of Club aeroplanes equipped with GPS systems that comply with the

requirements of this sub-section, should insert the following in flight plans:

(a) DOMESTIC FLIGHT NOTIFICATION; circle "Z" in field 10, and

"NAV/GPSRNAV" in Item 18(b); or

(b) ICAO FLIGHT PLAN; "Z" in field 10, and "NAV/GPSRNAV" in field 18.GG

© AEROSERVICE 2000

08/00 THE REDCLIFFE AERO CLUB Section A1

GENERAL Appendix 1

Page 1

AIR OPERATORS' CERTIFICATE

© AEROSERVICE 2000


GENERAL Appendix 2

Page 1

CAR 215 DIRECTIONS, PERMISSIONS AND APPROVALS

AMD 15


03/09 THE REDCLIFFE AERO CLUB Section A1GENERAL Appendix 3

Page 1

NAMES AND CONTACT TELEPHONE NUMBERS

POSITION/ORGANISATION NAME PHONE FAX

The Redcliffe Aero Club Reception 07 3203 1777 07 3203 3514

CEO Tony Stanton07 3283 84670435 032 357

07 3203 3514

Chief Pilot Tony Stanton 07 3203 1777 07 3203 3514

L CFI Tony Stanton 07 3203 1777 07 3203 3514

HAAMC Lee Goodrich 07 3203 1777 07 3203 3514

Safety Officer Mal McAdam 07 3203 1777 07 3203 3514

L DAMP Contact Tony Stanton 07 3203 1777 07 3203 3514

L DAMP Supervisor Tony Stanton 07 3203 1777 07 3203 3514

Maintenance OrganisationFlinders Aviation

Michael Kelly07 3203 0560

Vintage Aircraft ServicesPatrick Harrington

07 3293 1333

L Rapair 07 3277 7877

L AMS 07 5491 6819

Interactive Voice Response 1800 805 150

Flight Plans 1800 805 150 02

NAIPS 019 830 4767

Dectalk BrisbaneMelbourne

1800 077 2761800 034 454

Cancel SAR Censar 1800 814 931

National Help Desk 1800 801 960

Search and Rescue Hotline 1800 815 257

L The NAIPS Internet Access Client program is available for download athttp://www.airservices.gov.au/brief/iecs.asp

LAirservices briefing is available on the Internet at;http://www.airservices.gov.au/brief/default.asp



GENERAL Appendix 3

Page 2

NAMES AND CONTACT TELEPHONE NUMBERSDIRECTORS / MANAGEMENT COMMITTEE 2009

PRESIDENT / TREASURER:

L Greg McCallum 87 Payne Street H: 3870 8561AUCHENFLOWER QLD 4066 M: 0409 635 854Email: [email protected]

VICE PRESIDENT:

L Stephen White 24 Seventh Ave H: 3851 2785WINDSOR QLD 4030 W: 3229 7444Email: [email protected] M: 0418 980 172

SECRETARY:

L Ryan Scott PO Box 207 H: 3263 7323ASPLEY QLD 4034 M: 0414 872 096Email: [email protected]

GENERAL COMMITTEE:

L Ron Ennis 41 Morris Road H: 32033840ROTHWELL QLD 4022 M: 0414 883 864Email: [email protected]

L Ray Vuillermin 134 Cedar Creek Rd H: 3289 4292CLOSEBURN 4520 M: 0409 584 574Email: [email protected]

L Shane Wise 554 Robinson Rd H: 3862 7017ASPLEY QLD 4034 M: 0466 364 291Email: [email protected]

L Matthew Millitano 20 Pituri St H: 3261 3346BRACKEN RIDGE QLD 4017 M: 0401 056 445Email: [email protected]

L Duncan Greer 36 Mordant StASCOTT QLD 4007 M 0403 381 681Email: [email protected]

L CEO / CP / CFI:

Tony Stanton Email: [email protected] H: 3482 3099CP / CEO / CFI M: 0435 032 357Rob Beaumont Email: [email protected] H: 3203 3515

Asst. CFI M: 0428 435 863

LNote: Where Directors listed change mid-term, an up-to-date list is available atwww.redcliffeaeroclub.com.au in the contact Section.



GENERAL Appendix 3

Page 3

THE AIRSERVICES PHONEAWAY CARD MENU OPTIONS

MENUOPTION

FEATURE SERVICE

*01 Pilot BriefingVoice

This option takes users directly through to staff in the Briefing Officewhere you can:• Obtain pilot briefing material and/or• Submit a flight plan

*02 Pilot BriefingFacsimile

This option is to submit a flight plan via the fax.

*03 Pilot BriefingChange Request

Use this option when you need to make a change to a flight plan,cancel a flight plan, or confirm that your flight plan sent by fax hasarrived at the Briefing Office.

*04 AVFAX Pilot briefing material from the fax back system.

*05 DECTALK Digitised voice recordings of weather information

*06 PublicationsCentrepurchase a newPhoneAwayCard

This options takes users through to Airservices Publications Centrewhere you can order:• PhoneAway cards• Aeronautical publications such as the AIP, to En Route Supplement,

instrument and visual maps and charts.

*07 Credit CardRefresh

Use this option to top up the credit balance on your PhoneAway card. Remember to have your credit card ready and that only one credit cardcan be used for each PhoneAway card.

*08 Voicemail Use this option if you wish to access the Voicemail feature of the card

*09 Fax Messaging Use this option if you wish to access the Fax messaging feature of thecard

*10 Repeat themenu

Go back and listen to the menu options menu again

OR Enter thenumber to becalled

Simply enter the number you wish to call, using the full numberincluding the area code for all calls

OR Hold on the line You will be connected with Airservices Australia's Help Desk



GENERAL Appendix 4

Page 1


CREW MEMBER EMERGENCY PROFICIENCY TEST

NAME: DATE: AIRCRAFT TYPE:

PRACTICAL SIGNATURE

EMERGENCY EVACUATION PROCEDURES

DOOR - OPERATION

EMERGENCY EXIT - OPERATION

FIRE EXTINGUISHING EQUIPMENT

- LOCATION OF EQUIPMENT

- METHOD OF OPERATION

FIRST AID KIT

- CONTENTS

- LIMITATION OF USE

- PRECAUTIONS


DITCHING PROCEDURE

L LIFEJACKETS

- FITTING

- METHOD OF INFLATION

L - INITIAL QUALIFICATION - DEMONSTRATE COMPETENCY OF USE IN WATER

LIFERAFTS

- METHOD OF INFLATION

L - INITIAL QUALIFICATION - DEMONSTRATE COMPETENCY OF USE IN WATER

SIGNALLING EQUIPMENT


- METHOD USE



Page 2


THEORETICAL SIGNATURE

FIRE EXTINGUISHING EQUIPMENT

- TYPES

- USE

FIRST AID KIT

- CONTENTS

- LIMITATIONS OF USE

- PRECAUTIONS

L FLOTATION DEVICES

SURVIVAL


METHODS - LAND

- WATER

PASSENGER CONTROL

- METHODS OF CONTROL

- STORAGE/USE OF EQUIPMENT

- HANDLING DERANGED PASSENGERS

- HIJACKINGS

CERTIFICATE OF PROFICIENCY

NAME: ARN:

HAS (IN ACCORDANCE WITH CAO 20.11) SATISFACTORILY COMPLETED THE

CREW MEMBER EMERGENCY PROFICIENCY TEST

FOR THE TYPE AIRCRAFT.

DATE: SIGNED POSITION

© AEROSERVICE 2000


Page 1THE REDCLIFFE AERO CLUB

AEROPLANE LANDING AREA DESCRIPTION

PLACE NAME:

OWNER/OCCUPIER'S NAME & ADDRESS:

TELEPHONE NUMBER:

LOCATION OF LANDING AREA (LAT./LONG., DISTANCE/BEARING FROM NEAREST TOWN AND/OR HOMESTEAD,ETC.):

TYPE OF LANDING AREA (AIRSTRIP/ALL-OVER FIELD/ETC.):

SURFACE DESCRIPTION (GRASS/SOIL-TYPE/GRAVEL/CLAY PAN, ETC.):

SURFACE CHARACTERISTICS, FEATURES, HAZARDS:

DESCRIPTION, HEIGHT, DISTANCE, DIRECTION OF OBSTRUCTIONS THAT MAY AFFECT APPROACHES, LANDINGS,AND TAKE-OFFS:

AIRFIELD MARKINGS: YES/NO: TYPE:

AIRFIELD ELEVATION AMSL: WINDSOCK: YES/NO, POSITION:

LENGTH OF LONGEST STRIP: DIRECTION OF LONGEST STRIP:

LENGTH OF ANY OTHER: DIRECTION OF ANY OTHER:

POSSIBILITY OF LIVESTOCK ON LANDING AREA: YES/NO, DETAILS:

ESTIMATED NUMBER OF POINTS OF RAIN TO RENDER AREA UNSERVICEABLE:

AVIATION FUEL AVAILABLE? YES/NO: GRADE: AVGAS/AVTUR; QUANTITY:

DRUMMED/BOWSER; FUELLING INFORMATION:

MAY AIRCRAFT LAND WITHOUT SPECIFIC PERMISSION FOR EACH FLIGHT: YES/NO:

IF YES: AUTHORISATION GRANTED BY:

OPERATING APPROVAL AND/OR PRE-FLIGHT REPORT (NAME/PHONE NO.):

ADDITIONAL INFORMATION:

DETAILS VERIFIED BY: DATE:

SKETCH/DIAGRAM (USE REVERSE SIDE)

© AEROSERVICE 2000


GENERAL Appendix 5

Page 2


ALA REGISTER

INDEX

No. TITLE

1.

2.

3.

4.

5.

6.

7.

8.

9.

10.

11.

12.

13.

14.

15.

16.

17.

18.

19.

20.




SECTION A2

FLIGHT CREW ADMINISTRATION

SUB-SECTION PAGE

2.1 PILOT RECORDS A2-3

2.2 FLIGHT TIME RECORDS A2-3

2.3 PILOT ROUTE QUALIFICATIONS A2-5

2.4 INDUCTION AND TRAINING REQUIREMENTS A2-5

2.5 AIRCRAFT TYPE ENDORSEMENTS A2-6

2.6 MINIMUM EXPERIENCE REQUIREMENTS A2-7

2.7 RECENCY REQUIREMENTS A2-8

2.8 DUTY AND FLIGHT TIME LIMITATIONS A2-9

2.9 ROSTERING SYSTEM A2-13

2.10 PILOTS OVER THE AGE OF 60 A2-14

2.11 TEMPORARY MEDICAL UNFITNESS A2-15

2.12 INELIGIBILITY TO FLY A2-15

2.13 AIR TRANSPORT PILOT LICENCE A2-15

2.14 INSTRUMENT RATING REQUIREMENTS A2-16

2.15 NON-CASA QUALIFICATIONS A2-16

L 2.16 TRAINING FOR MAINTENANCE AUTHORITY APPROVAL A2-17



03/06 FLIGHT CREW ADMINISTRATION A2-2

SECTION A2

FLIGHT CREW ADMINISTRATION

APPENDIXES:

1. PILOT RECORD

2. DUTY/FLIGHT TIME & EXPERIENCE RECORD

3 INDUCTION RECORD

4. CERTIFICATE OF TRAINING FOR MAINTENANCE AUTHORITY APPROVAL

5. PILOT MAINTENANCE TRAINING CERTIFICATE

L 6. PILOT ROSTER

L 7. BOOKING SHEET


© AEROSERVICE 2000


2.1 PILOT RECORDS

(1) The Chief Pilot shall maintain up to date personal records for each flight crew

member employed by the Club, irrespective of whether such employment is

on a full time or part time basis. The information shall include the type and

expiry dates for;

(a) flight crew licence

(b) medical certificate;

(c) any condition imposed by CASA on ratings held by the pilot;

(d) Club training;

(e) external training, including the name of the organisation or individual

conducting external training.

(2) The records shall contain photocopies of the relevant records and certificates.

(3) The pilot's personal records shall only be open to inspection by:

(a) the crew member concerned, in the presence of the Chief Pilot or

delegate; or

(b) an authorised officer of the Civil Aviation Safety Authority, in the

presence of the crew member concerned and the Chief Pilot or delegate;

or

(c) with the approval of the pilot concerned, an authorised Aviation Audit

officer on behalf of a Club client, in the presence of the Chief Pilot.

(4) A copy of the Club's Pilot Record is shown as Appendix 1 to this Section.

2.2 FLIGHT TIME RECORDS

(1) The Club and its flight crew members share responsibility to ensure that duty

and flight times as laid down in sub-section 2.8 of this section (including any

variations authorised under an exemption which may be granted by CASA) are

not exceeded. A flight crew member is to notify the Chief Pilot as soon as it

becomes apparent that flight or duty times might be exceeded. ....




2.2 FLIGHT TIME RECORDS

(2) Newly recruited (including part-time) pilots shall not be employed as a member

of the operating crew of any Club operated aircraft unless they confirm by

presentation of an up to date personal log book and/or a current duty and

flight time record or similar document that sufficient flight and duty time is

available for the proposed operation.

(3) Upon completion of each tour of duty, Club pilots will enter flight time and duty

period for that day together with any other relevant data into his/her current

Duty/flight Time & Experience Record including the CASA concession number

if the pilot has exceeded the provisions of sub-section 2.8 of this Section in

any particular while engaged in commercial operations.

L (4) A Club pilot’s record of flight/duty time and experience shall be in the format

shown at Appendix 2 to this Section. This must be calculated and completed

manually using either a pen, a computer spreadsheet or commercially

available computer software. A pilot may use commercially available duty time

software only after approval of the Chief Pilot. The format produced by the

software may be different to Appendix 2 but needs to display the same

information as agreed with the Chief Pilot. The Club pilot is responsible to

ensure the software correctly calculates information when presented to the

Chief Pilot.

(5) The flight time recorded shall be the total time entered for that particular day

as “PILOT FLIGHT TIME” on the Passenger Manifest and Flight Record for the

aircraft for which that pilot was a crew member. Refer to page AO-6 for the

definition of "Flight Time"

(6) A copy of the Club's Passenger Manifest and Flight Record is shown at

Appendix 1 to Section A4.





2.3 PILOT ROUTE QUALIFICATIONS

(1) Before the Chief Pilot rosters a flight crew member to act as flight crew of aaeroplane engaged in charter operations, he/she shall ensure that;

(a) the pilot has operated over that route or, if the operation type operation,has conducted operations in that area; or

(b) if the pilot has not operated over the route or in the area, the Chief Pilotshall ensure that the pilot is briefed on the following;

(i) the terrain in the area of the intended operation;

(ii) the weather conditions to be expected;

(iii) the aerodromes and or ALAs to be used;

(iv) if low level operations are to be conducted, hazards known to exist;

(v) SAR procedures to be used by the pilot, i.e. Airservices or Clubflight following; and

(vi) if the flight is conducted under the IFR, has demonstrated in flightor in a synthetic trainer, proficiency and currency in the type ofinstrument approaches that may be utilised in the conduct of theflight.

2.4 INDUCTION AND TRAINING REQUIREMENTS

(1) The Chief Pilot will determine the suitability, qualifications, appropriatelicence/ ratings and experience of a pilot before he/she is engaged by theClub

(2) The Chief Pilot or delegate shall complete an Induction Record for all newlyrecruited pilots.

(3) It shall be the responsibility of the Chief Pilot to ensure that before any pilotis rostered to fly as pilot in command of a Club aeroplane that pilot's personalrecord is complete and that pilot:

L (a) has the required qualifications and piloting standards specified in sub-section 2.6, this Section;

(b) meets the applicable recency provisions specified at sub-section 2.7(1),this Section;

L (c) has within the previous 24 months, satisfactorily completed an aeroplaneflight review in accordance with sub-section 2.7(2) or, if over the age of60 years, meets the requirements of sub-section 2.10;

....




2.4 INDUCTION AND TRAINING REQUIREMENTS

(3) It shall be the responsibility of the Chief Pilot to ensure that ... (Cont’d):

(d) has, within the previous 27 months, completed the applicable training inrelation to dangerous goods as detailed in sub-section 8.3 of Section A8;

(e) has completed the emergency procedures training and has been issuedwith a Certificate of Proficiency specified in sub-section 1.13 of SectionA1;

(f) has satisfactorily completed the Club training for loading, cargo restraintand pilot maintenance for the particular aeroplane type and whererequired by the Club, training under sub-section 2.16;

L (g) meets the requirements of the Company's Drug and AlcoholManagement Plan;

(h) has studied the Club's Operation Manual and, by oral evaluation, isthoroughly familiar with all relevant operational procedures andpractices; and

(i) has signed the signature sheet in the appropriate copy of the Club'sOperations Manual as evidence of having read, understood and agreedto apply the procedures contained therein.

(4) Copies of the Club’s Pilot Record, the Induction Record and the PilotMaintenance Training Certificate are shown as Appendix 1, 3 and 5,respectively, to this Section.

2.5 AIRCRAFT TYPE ENDORSEMENTS

(1) If it becomes necessary for a pilot to be endorsed on a Club operatedaeroplane, the required conversion training and tests shall be carried out bya rated flight instructor who holds a valid commercial pilot (aeroplane) licenceendorsed for the type of aeroplane, or by the holder of a commercial or highercategory pilot (aeroplane) licence who has been approved by the Civil AviationSafety Authority to conduct endorsement training on the aeroplane typeconcerned.

(2) On the successful completion of the required training, the pilot shall ensurethat a CASA delegate inserts a "sticky strip" certification and details of theendorsement in the pilot's log book and forwards a copy of the endorsementcertificate to CASA.

(3) Club pilots, upon the successful completion of a endorsement, shall forwarda photocopy of the “Certificates of Endorsement on Aircraft Types, Classesand Design Features” Log Book page to the Chief Pilot who shall enter thedetails in that pilot’s Pilot Profile and retain the photocopy in file.


© AEROSERVICE 2000


2.6 MINIMUM EXPERIENCE REQUIREMENTS

(1) Aeroplanes not above 5700 kg MTOW

(a) Aerial Work (single/multi engine VFR/NVFR or IFR):

* Commercial Pilot (Aeroplane) Licence

* Type or group endorsement

* Ratings(s) as required

* Post-endorsement experience or training where stipulated in Part D

for those specialised operations in which the pilot will engage.

(b) Charter:

(i) Single-engine VFR



* 5 hours as pilot in command on type

(ii) Single-engine IFR



* 5 hours as pilot in command on type

* Command (single-engine aeroplane) instrument rating

(iii) Multi-engine VFR


* Type endorsement with 5 hours as pilot in command on that

aeroplane type or 100 hours as pilot in command on multi-engine

aeroplanes

(iv) Multi-engine IFR


* Type endorsement

* Command (multi-engine aeroplane) instrument rating

* 10 hours as pilot in command on type which may include flight

time accrued while acting as pilot in command under supervision


© AEROSERVICE 2000


2.7 RECENCY REQUIREMENTS

(1) A pilot shall not act as pilot in command of a Club aeroplane carrying

passengers unless he/she has within the preceding 90 days either carried out at

least three take-offs and landings while acting as pilot in command or as pilot in

command under supervision, or in dual flying, or has passed a flight test (a flight

proficiency check, a flight test for the issue of an aeroplane pilot licence, or the

issue or renewal of a pilot rating) by a CASA Flying Operations Inspector or an

approved testing officer, by day or night, as applicable.

(2) A pilot shall not act as pilot in command of a Club aeroplane unless he/she

has within the previous 24 months;

(a) satisfactorily completed a aeroplane flight review and an entry made to

that effect in the pilot's personal log book by the person who conducted

the review; or

(b) has satisfactorily completed the issue, or renewal, of an aeroplane pilot

rating; or

(c) has satisfactorily completed aeroplane conversion training given by the

holder of a flight instructor (aeroplane) rating that authorises that

instructor to conduct flight reviews.

Club pilots, upon the successful completion of either (a), (b) or (c) above, shall

forward a photocopy of the Log Book page containing the endorsement for the

flight review to the Chief Pilot who shall enter the details in that pilot’s Pilot

Record.



© AEROSERVICE 2000


2.8 DUTY AND FLIGHT TIME LIMITATIONS

(1) Private and Commercial Operations

The intent of the following paragraphs is to preserve the integrity of the flight

and duty time limitations applied to commercial operations to ensure the

observation of the safety standards as stated in CAO 48.

(a) Where a Club pilot engages in a mix of commercial and private

operations, all flight and duty time associated with the private operation

shall be taken into account in determining compliance with the flight and

duty time limitations specified for commercial operations.

(b) If private operations are carried out immediately prior to commencing a

period of commercial operations or are sandwiched between periods of

commercial operations, then the full amount of both flight and duty times

incurred during the period of private operations must be accounted for

on the applicable flight and duty time record.

(c) If private operations are carried out immediately after a commercial tour

of duty the pilot can continue to fly on private operations irrespective of

total flight or duty time. If extended flight or duty time is undertaken on

private operations, an extended rest period may be required before the

pilot is available to be rostered for either a tour of duty or reserve time

at home. The full amount of both flight and duty times incurred during the

period of private operations must be accounted for on the applicable

flight and duty time record.

(2) Flight Hours Limits

The limits which apply to Club pilots engaging in charter and aerial work

operations are:

(a) 900 hours in 365 consecutive days

(b) 100 hours in 30 consecutive days

(c) 30 hours in 7 consecutive days.

....


© AEROSERVICE 2000



(3) Duty Hour Limits

The Club shall not roster a pilot for a total of more than 90 hours duty time in

each fortnight standing alone. A Club pilot shall not commence a period of

duty if, at the end of the duty period, the pilot will exceed 90 hours duty time

in the current fortnight period. The Club shall nominate the day on which the

first of the fortnightly periods shall start. This day shall be nominated on the

Club's roster.

(4) Pre-flight and Post-flight Activities

Pre-flight and post-flight activities by flight crew associated with a commercial

operation must be included as an integral part of crew duty time in assessing

duty time limitations. For planning purposes, a minimum allowance of 45

minutes for charter operations or 15 minutes for training operations shall be

added before and 15 minutes after the anticipated duty time to allow for pre-

flight and post-flight activities.

(5) Reserve Time

(a) The maximum allowable continuous time on reserve duty at home is 16

hours.

(b) The maximum allowable duty period following call out from standby shall

not exceed 23 hours. This maximum shall include the completed standby

duty period.

(6) Dead Head Transportation

When a Club pilot is required to travel for Club purposes to commence a

period of duty and that travel is not followed by a prescribed rest period in

accordance with sub-section (7) below, the travel time and duty period shall

count as a tour of duty. Where the travel was conducted after the tour of duty

and was not preceded by a prescribed rest period in accordance with sub-

section (7) below, the travel time and duty period shall count as a tour of duty

for the purposes of calculating the required rest period preceding a the next

tour of duty. ....





(7) Duty and Rest Periods

(a) The normal rostered tour of duty will be 11 hours including a maximumof 8 hours flight time.

L (b) A rest period preceding a tour of duty or reserve time at home shall beat least;

(i) 9 consecutive hours covering the period 2200 hours to 0600 hoursLMT;

(ii) 9 consecutive hours, if the aircraft is scheduled to arrive to enablethe pilot to finish the duty period before 2200 hours LMT and theaircraft is delayed beyond 2200 hours LMT, the rest time may becommenced up to 2300 hours LMT provided the next tour of dutydoes not exceed 6 hours; or

(iii) 10 consecutive hours.

(c) Where a pilot has completed two consecutive tours of duty, theaggregate of which exceeds 8 hours flight time or 11 hours duty time,and the intervening rest period is less than -

(i) 12 consecutive hours embracing the hours between 2200 and 0600time; or

(ii) 24 consecutive hours if not embracing the hours between 2200 and0600 time;

- that pilot shall have a rest period on the ground, of at least 12consecutive hours of which includes the hours between 2200 and 0600local time alternatively 24 consecutive hours, prior to commencing afurther tour of duty; or

(iii) if the aircraft is scheduled to arrive to enable the pilot to finish theduty period before 2200 hours LMT and the aircraft is delayedbeyond 2200 hours LMT, the rest time referred to in (I) above maybe commenced up to 2300 hours LMT provided the next tour of dutydoes not exceed 6 hours;

(d) in any seven-day period, a pilot must be off duty for at least onecontinuous period covering the hours between 2200 and 0600 on twoconsecutive nights. ....


© AEROSERVICE 2000



(8) Extensions of Flight or Duty Periods

(a) A tour of duty already commenced may be extended to 12 hours subjectto an extra rest period on the ground of not less than:

(i) nine consecutive hours which shall include the hours between 2200and 0600 local time, plus one additional hour for each fifteenminutes or part thereof by which his/her tour of duty time exceededeleven hours; or

(ii) ten consecutive hours plus one additional hour for each fifteenminutes or part thereof by which his/her tour of duty time exceededeleven hours.

(b) For VFR operations, a pilot may be rostered for a tour of duty notexceeding 15 hours provided that;

(i) a break of 4 consecutive hours where the pilot is free of all dutiesassociated with his/her employment is included in the 15 hours;

(ii) a rest period of 24 hours is allowed between any two consecutivetours of duty which each exceed 11 hours;

(iii) no more than two tours of duty exceeding 11 hours are rostered inany six consecutive days;

(iv) no more than six hours of flight instruction are rostered in a tour ofduty which exceeds 11 hours.

(c) Flight time already commenced within a duty period may be extended toa maximum of 9 hours subject to an extra rest period on the ground ofnot less than:

(i) nine consecutive hours which shall include the hours between 2200and 0600 local time, plus one additional hour for each fifteenminutes or part thereof by which his/her flight time exceeded eighthours; or

(ii) ten consecutive hours plus one additional hour for each fifteenminutes or part thereof by which his/her flight time exceeded eighthours;

(d) CASA may from time to time approve an application for a variation ofdaily, weekly and monthly duty or flying hours for Club pilots engagingin specific operations. Refer to sub-section 1.2 Section A1 forapplicability. ....





(9) FITNESS FOR FLIGHT CREW DUTIES

(a) A flight crew member shall not operate an aircraft and the Club shall notrequire or permit a flight crew member to operate an aircraft unless atthe commencement of any duty period:

(i) the flight crew member has taken adequate rest;

(ii) the flight crew member has taken adequate sustenance; and

(iii) the flight crew member is free of any fatigue, illness, injury,medication or drug which could impair the safe exercise of his orher licence privileges.

(b) When a Club pilot is required to undertake a rest period away fromhis/her home base, the Club shall provide for and a pilot shall ensurethat adequate rest is taken during the rest period prior to commencingor recommencing duty.

(10) Standown

(a) If the flight or duty times limits of a Club pilot will be exceeded, the Clubshall not roster that pilot to fly until he/she has sufficient duty or flighthours available;

(b) The Club may roster a pilot for duties other than flight duties in excessof the time specified in 2.8(3) above. The pilot concerned shall not berostered to fly until he/she has sufficient duty and flight hours available.

2.9 ROSTERING SYSTEM

(1) Before rostering a pilot for duty, the Chief Pilot shall ensure that the pilot;

(a) is qualified to act as pilot in command of the aeroplane and the pilot'slicence, ratings and medical certificate is valid for the period of theroster;

(b) meets recency requirements;

(c) if conducting charter operations, is qualified to act as pilot in commandover the route;

(d) meets the aeroplane flight review requirements;

(e) has met the requirements for emergency procedures;

(f) has sufficient flight time and duty hours.

(2) Club pilots shall notify the Chief Pilot if it appears that the flight or duty timesindicated on the pilot's roster will exceed any provisions of sub-section 2.8.

(3) The Chief Pilot shall ensure that a pilot duty roster is prepared for a period of14 days at least 7 days in advance.

....




2.9 ROSTERING SYSTEM

(4) The duty roster will show the 'duty days' and the 'duty free days' allocated toeach pilot during the period covered by that roster. However, pilots areadvised that the roster may be subject to alteration at short notice due tooperational factors such as staff illness, weather, cancellations and othercircumstances beyond Club control.

L (5) For all permanent pilots a standard 14 day roster in the format shown atAppendix 6 of this section shall be prepared and presented to each club pilot.This roster shall be taken to occur on a continually rotating basis. The rosterso presented may be amended per sub-section 2.9(4) above in the form ofchanges to the “booking sheet” system (format shown at Appendix 7 of thissection). A pilot’s “regular hours” are first entered onto the booking sheets withRDOs etc ruled out. When a change becomes necessary the booking sheetis changed in advance to act as an amended roster. All changes must bemade in consultation with the Chief Pilot, though permanent pilots may self-authorise changes in the Chief Pilot’s absence, if certain that no breach ofCAO 48 will occur.

(6) The pilots duty roster shall be clearly identified with the various CASAconcessions which provide authority for pilots to exceed certain flight and/orduty requirements specified in CAO 48.1 and which are being utilised in thatparticular roster period.

2.10 PILOTS OVER THE AGE OF 60

(1) The Chief Pilot shall not authorise a pilot who is passed his/her 60th birthdayto act a pilot in command of a Club operated aeroplane on commercialpassenger carrying operations unless;

(a) the pilot flies an aeroplane which has fully functioning dual controls anda second qualified pilot who is less than 60 years old is carried andoccupies a control seat; or

(b) if the pilot is less than 65 years old, that pilot has, within the period ofone year immediately before the date of the proposed flight, satisfactorilycompleted an aeroplane flight review; or

(c) if the pilot is at least 65 years old, that pilot has, within the period of sixmonths immediately before the date of the proposed flight, satisfactorilycompleted an aeroplane flight review.

(2) The pilot referred to in (1) above upon the successful completion of anaeroplane flight review, shall forward a photocopy of the “Flight Check andApprovals” Log Book page to the Chief Pilot who shall enter the details in thatpilot’s Pilot Record.


© AEROSERVICE 2000


2.11 TEMPORARY MEDICAL UNFITNESS

(1) Club pilots are not to fly while suffering an incapacity resulting from any form

of illness or injury, however minor or temporary, which is likely to impair their

efficiency in performing flight duties. Pilots are to advise the Chief Pilot as

soon as practicable following the onset of any incapacity which is likely to

impair their efficiency in performing flight duties.

(2) Where a Club pilot, through medical unfitness, is unable to perform his/her

flight duties for a period of seven days or more, that pilot is to obtain a

certificate from a designated aviation medical examiner that the impairment

no longer exists before performing duties as a flight crew member on Club

aircraft.

2.12 INELIGIBILITY TO FLY

(1) Club pilots are not to fly while ineligible to do so. This ineligibility may be due

to recency requirements, qualifications, CAO 48 requirements, medical or

personal problems.

(2) Where a Club pilot considers that he/she may be ineligible to fly, he/she is to

consult the Chief Pilot.

2.13 AIR TRANSPORT PILOT LICENCE

As Club operations do not require pilots employed by the Club to hold an Air

Transport Pilot (Aeroplane) Licence, Club pilots, who hold an Air Transport Pilot

(Aeroplane) Licence may conduct any operation for which a Commercial Pilot

(Aeroplane) Licence is Club requirement.





2.14 INSTRUMENT RATING REQUIREMENTS

(1) Club pilots rostered as pilot in command to conduct single-engine or multi-engine operations under the IFR shall hold a command (single-engine ormulti-engine aeroplane as applicable to the aeroplane type) instrument ratingand have, as a minimum, endorsements in his/her log book for the followingnavigation aids or procedures;

(a) NDB;

(b) DME or GPS arrival procedure.

(2) The holder of a instrument rating referred to in (1) above may act as a co-piloton Club aeroplanes, for which that pilot has a type or class endorsement,while conducting operations under the IFR.

(3) The recency requirements of sub-section 6.7 of Section A6 appropriate to thenavigation aid or procedure intended to be used shall be met before a Clubpilot shall conduct operations under the IFR.

2.15 NON-CASA QUALIFICATIONS

(1) Special Pilot Licence

Holders of an overseas pilot licence may apply to CASA for the issue of aSpecial Pilot Licence. Before the holder of a Special Pilot Licence may fly aspilot in command of Club aeroplanes, he/she shall;

(a) hold an endorsement for the aeroplane type;

(b) hold a valid and current medical certificate or a valid and currentoverseas medical certificate;

(c) pass at a minimum, a flight review conducted by the CFI;

(d) only conduct private operations.

(2) Certificate of Validation

Holders of an overseas qualification may apply to CASA for the issue of aCertificate of Validation. Before the holder of a Certificate of Validation mayfly as pilot in command of Club aeroplanes, he/she shall;

(a) hold an endorsement for the aeroplane type;

(b) hold a valid and current medical certificate or a valid and currentoverseas medical certificate;

(c) pass at a minimum, a flight review conducted by the CFI.




2.16 TRAINING FOR MAINTENANCE AUTHORITY APPROVAL

L (1) To enable a Club pilot to conduct specific maintenance on Club aeroplanes

other than as allowed under Schedule 8 of the CAR, the Chief Pilot shall request

the Chief Engineer of the Club’s maintenance organisation to conduct the

training of the pilot for the maintenance to be conducted.

(2) The Chief Engineer shall determine the extent of the training required based

on the pilot’s experience and qualifications.

(3) On the successful completion of the training, the Chief Engineer shall

complete a Certificate of Training for Maintenance Authority Approval in

duplicate.

L (4) One copy shall be retained by the Club in the pilots’ record, the second shall

be submitted to the CASA along with a written application for approval under

CAR 42ZC(3)(d) and 42ZC(6).

(5) A copy of the Certificate of Training for Maintenance Authority Approval is

shown at Appendix 4 to this Section. GG

© AEROSERVICE 2000


FLIGHT CREW ADMINISTRATION Appendix 1

Page 1


PILOT RECORD

NAME: ARN:

ADDRESS:

TELEPHONE: DATE OF BIRTH:

FLIGHT CREW LICENCE: APPOINTMENT:

NEXT OF KIN:-

RELATIONSHIP: NAME:

TELEPHONE: ADDRESS:

ENDORSEMENTS:

SPECIALISED OPERATIONS:

SICK LEAVE HOLIDAY LEAVE SPECIAL LEAVE

START FINISH START FINISH START FINISH


01/05 THE REDCLIFFE AERO CLUB Section A2FLIGHT CREW ADMINISTRATION Appendix 1


PILOT RECORD

NAME: ARN:

AEROPLANE FLIGHT

REVIEWRATINGS

DANGEROUS GOODS

TRAININGMEDICAL CAO 20.11

L TYPE DATE DUE TYPE DATE DUE GROUP DATE DUE CLASS DATE DUE A/C TYPE DATE DUE



Page 1

L



Page 1


INDUCTION RECORD

NAME: ARN:

ITEM PHOTOCOPIED ENTERED VALID TO

PERSONAL RECORD SHEET

IDENTIFICATION SIGHTED

FLIGHT CREW LICENCE

MEDICAL CERTIFICATE

CASA RECORD OF FLIGHT CREW QUALIFICATIONS

LOG BOOK - CERTIFICATES OF ENDORSEMENTS

LOG BOOK - CERTIFICATES OF RATINGS

LOG BOOK - FLIGHT CHECKS AND APPROVALS

LOG BOOK - THEORY EXAMINATION PASS RECORD

FLIGHT REVIEW REQUIREMENTS

DANGEROUS GOODS TRAINING

EMERGENCY PROCEDURES TRAINING

CERTIFICATE OF PROFICIENCY ISSUE

FLIGHT AND DUTY RECORDS

RECENCY REQUIREMENTS

LOW FLYING CERTIFICATE

L AOD TRAINING AND TESTING

OPERATIONS MANUAL REVIEW

INSTRUMENT APPROACH AIDS (DELETE AIDS FOR WHICH THE PILOT IS NOT QUALIFIED)

ILS VOR NDB DME/GPS GPS NPA

I certify that the above records presented are a true and accuraterecords of my previous training, flying experience and qualifications.

Signature: Date:

I certify that has met the induction requirements of this Club andmay act as pilot in command on the aircraft listed below. I have personally checked the recordspresented and have completed the above pilot’s Pilot Record.

Signature: Date:

Aircraft Types:



L FLIGHT CREW ADMINISTRATION Appendix 4

Page 1


CERTIFICATE OF TRAINING FOR MAINTENANCE AUTHORITY APPROVAL

(Name) (Position)

On behalf of , I certify that

(Pilots Name) (ARN)

has been instructed in

and I believe he/she is competent to conduct the maintenance detailed above on the followingaeroplane type(s)

(Signature) (Licence No) (Date)

(Position) (Company)

GG

© AEROSERVICE 2000


FLIGHT CREW ADMINISTRATION Appendix 5

Page 1


PILOT MAINTENANCE TRAINING CERTIFICATE

This is to certify that holder of pilot licence type ARN

has satisfactorily completed training on the following items for aeroplane type

as indicated by a signature against that Item.

ITEM SIGNATURE

1 Removal or installation of landing gear tyres.

2. Repair of pneumatic tubes of landing gear tyres.

3. Servicing of landing gear wheel bearings.

4. Replacement of defective safety wiring or split pins, but not including wiring orpins in control systems.

5. Removal or refitting of a door.

6. Replacement of side windows in an unpressurised aircraft.

7. Replacement of seats, but only if the replacement does not involvedisassembly of any part of the primary structure of the aircraft.

8. Repairs to the upholstery or decorative furnishings of the interior of the cabinor cockpit.

9. Replacement of seat belts or harnesses.

10. Replacement or repair of signs and markings.

11. Replacement of bulbs, reflectors, glasses, lenses or lights.

12. Replacement, cleaning, or setting gaps of, spark plugs.

13. Replacement of batteries.

14. Changing oil filters or air filters.

15. Changing or replenishing engine oil or fuel.

16. Lubrication not requiring disassembly or requiring only the removal of non-structural parts, or of cover plates, cowlings and fairings.

17. Replenishment of hydraulic fluid.

18. Application of preservative or protective materials.

19. Removal or replacement of equipment used for agricultural purposes.

20. Removal or replacement of glider tow hooks

21. Carrying out of an inspection of a flight control system that has beenassembled, adjusted, repaired, modified or replaced.

22. Carrying out of a daily inspection of an aircraft.

23 Use of Maintenance Release

24 Loading and cargo restraint.

Pilot Signature: CP/LAME Signature:


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Page 1




SECTION A3

AIRCRAFT ADMINISTRATION

SUB-SECTION PAGE

3.1 USE OF MAINTENANCE RELEASE A3-3

3.2 METHOD OF RECORDING UNSERVICEABILITIES A3-4 3.3 AUTHORITY OF PILOT FOR MAINTENANCE A3-5

3.4 AUTHORITY OF MAINTENANCE PERSONNEL A3-6

3.5 FUEL DOCUMENTATION A3-6

3.6 FUEL USAGE RECORDS A3-7

3.7 PERSONS PERMITTED TO TAXI AIRCRAFT A3-7

3.8 PERSONS PERMITTED TO OPERATE CONTROLS A3-7

3.9 PROCEDURE IN EVENT OF UNSERVICEABILITY AWAYFROM HOME BASE A3-8

3.10 MAINTENANCE AND SERVICING OF AIRCRAFTAND AIRCRAFT COMPONENTS A3-8

3.11 CARRIAGE OF PERSONS IN SEATS AT WHICH DUALCONTROLS ARE FITTED A3-15

3.12 STARTING AND GROUND OPERATIONS OF ENGINES A3-16

3.13 GROUND OPERATION OF WEATHER RADAR A3-17

3.14 AIRCRAFT COMPONENT CONTROL A3-17

3.15 PORTABLE ELECTRONIC DEVICE A3-19

3.16 EMERGENCY EQUIPMENT RECORD A3-19

L 3.17 GPS DATABASE UPDATING A3-20....



04/04 AIRCRAFT ADMINISTRATION A3-2

APPENDIXES:

1. FUEL SHEET

2. CIVIL AVIATION REGULATIONS SCHEDULE 8

L 3. MAINTENANCE ADVISORY NOTICE and CofR HOLDER’S ADVISORY NOTICE

4 CROSS-HIRE AGREEMENT - AIRWORTHINESS CONTROL OF AIRCRAFT.

L 5. COMPONENT RECEIPT AND ISSUE REGISTER

L 6. EMERGENCY EQUIPMENT INSPECTION RECORD




3.1 USE OF MAINTENANCE RELEASE

(1) The Maintenance Release (CASA Form DA741) is made up of Parts 1, 2 and3. The Club shall ensure that copies of all Maintenance Releases are kept bythe issuing organisation for a minimum of 12 months and that all completedMaintenance Releases are permanently retained in the applicable aircraft logbook by the Certificate of Registration holder.

.(2) The Club shall ensure that any notification of suspension or cancellation of a

Maintenance Release for an aircraft for which the Club is the holder of theCertificate of Registration is passed to the Chief Engineer of the Club'smaintenance organisation and to flight crew who are rostered to fly thatparticular aircraft.

(3) PART 1

(a) This Part identifies the aircraft and class of operations for which theparticular Maintenance Release has been issued and among otherdetails pertinent to the issuing of that document, it expresses the periodfor which the Maintenance Release is to remain in force.

L (b) The lower half of this Part is for the purpose of making endorsements inrespect of requirements and conditions under the Civil AviationRegulations which will require maintenance, other than the dailyinspections, to be carried out on that aircraft during the period for whichthe Maintenance Release remains in force.

L (c) A signature, licence number and date adjacent to such an endorsementwill constitute a certification to the effect that the maintenance requiredto comply with that particular maintenance requirement has beencompleted and has been entered and certified for in the aircraft LogBook or Part 2 of this Maintenance Release.

(4) PART 2

(a) This Part is for the purpose of making endorsements in respect ofmaintenance requirements issued under the CARs, defective ordamaged components, abnormal flight or ground loads, maintenancecarried out which may have an adverse effect on the operation of theaircraft or any of its components.

(b) Each endorsement referred to in (4)(a) above, shall be numbered,signed and dated by the person making the endorsement

L (c) A signature, licence number and date adjacent to an endorsementconstitutes a certification clearing that endorsement, and/or that allmaintenance required to remedy the particular defect or damage hasbeen completed. ....


© AEROSERVICE 2000


3.1 USE OF MAINTENANCE RELEASE

(5) PART 3

(a) This Part is used to certify completion of the daily inspection pursuant toCivil Aviation Regulation 42ZE.

L (b) A signature, licence number and date in the columns provided for thepurpose constitutes a certification for completion of the daily inspectionon the date shown adjacent to that signature.

(c) Upon completion of each day's flying, entries with respect to aircraft timein service shall be made in the appropriate columns showing the totaltime flown and the total number of landings made in the course of thatday. This time shall be the daily total time between “DEPARTURE TIME”and “ARRIVAL TIME” as recorded on the Passenger Manifest and FlightRecord for that particular aeroplane. Refer to Page AO-6 for thedefinition of "Time in Service"

(d) A copy of the Club Aircraft Passenger Manifest and Flight Record isshown at Appendix 1 to Section A4.

3.2 METHOD OF RECORDING UNSERVICEABILITIES

L (1) If the pilot in command or the operator becomes aware of any damage to theaeroplane or any of the aeroplane’s systems, a maintenance requirementissued under the CARs, or he/she considers the aeroplane has acquiredcharacteristics such as to adversely affect the safety of that aircraft or anyother unserviceability of the aeroplane or its equipment which affects, or mayaffect, the satisfactory operation of that aeroplane, he/she shall make an entryin the 'Endorsements' column of Part 2 of the Maintenance Release setting outthe relevant particulars.

L (2) If an endorsement referred to in (1) details maintenance requirements issuedunder the CARs, major damage or a major defect, abnormal flight or groundloads or maintenance carried out which may have an adverse effect on theoperation of the aircraft or its flight characteristics or the operatingcharacteristics of its components or any of its systems and there is alikelihood that the aircraft will be flown before maintenance to rectify theendorsement is carried out, the person making the endorsement shall alsoendorse the Maintenance Release with the text "aircraft is unairworthy". TheMaintenance Release shall then cease to be in force.

....




3.2 METHOD OF RECORDING UNSERVICEABILITIES

(3) All endorsements made on the Maintenance Release shall be reported to anddiscussed with the Chief Pilot or delegate or, if unavailable, the Chief Engineerof the Club’s approved maintenance organisation to determine rectificationaction.

(4) The Chief Engineer shall investigate all defects and damage and take actionfor the correction of all defects and damage or make application to CASA forpermissible unserviceabilities or Special Flight Permits, whichever action isrequired to allow continued operation of the aircraft;

(5) The required maintenance for items referred to in (2) shall be carried out byan appropriately licensed aircraft maintenance engineer and when anendorsement is made in the “Clearing Endorsements” column on Part 2 of theMaintenance Release, the Maintenance Release shall again be in force.

(6) The pilot in command retains the right to refuse to commence a flight if he/sheis not entirely satisfied that the fault has been rectified or considers the aircraftto be unserviceable at the time of carrying out the subsequent daily or pre-flight inspection.

L (7) The HAAMC shall monitor endorsements, being endorsements that do notaffect safety of flight and are non-airworthiness related endorsements, toensure that they are rectified in a timely manner.

3.3 AUTHORITY OF PILOT FOR MAINTENANCE

(1) Under the provisions of CAR 42ZC(4)(d), a Club pilot, other than a studentpilot, is authorised to carry out the daily inspection on an aircraft of whichhe/she is the pilot in command.

(2) For all Club operated aeroplanes, the approved daily inspection is thatspecified in the Aircraft Log Book Statement Part 1 for each aeroplane.

(3) If the Chief Pilot or the Chief Engineer cannot be contacted and an aircraftmaintenance engineer is not readily available, the pilot in command isauthorised to carry out and certify any of the maintenance items specified inSchedule 8 of the Civil Aviation Regulations, as applicable to type for whichthat pilot has received specific training and has access to the manufacturer’smaintenance data and the applicable calibrated tooling. A copy of Schedule8 is shown as Appendix 2 to this Section.

(4) The Chief Engineer of the Club’s maintenance organisation shall instruct newinducted pilots on Schedule 8 maintenance items. This instruction shallinclude the requirements for the use of the applicable maintenance data andthe use of calibrated tools in the conduct of this maintenance. Uponcompletion of this training, the Chief Engineer shall complete a PilotMaintenance Training Certificate for that pilot. ....




3.3 AUTHORITY OF PILOT FOR MAINTENANCE

(5) A copy of the Pilot Maintenance Training Certificate is shown at Appendix 5to Section A2.

L (4) Except for an aircraft daily inspection and MR certification for that inspection,a student pilot may only complete maintenance items 15, 17 and 22 ofSchedule 8 of the Civil Aviation Regulations, while under the directsupervision of an Instructor. The Instructor carrying out the supervisionremains responsible for any such maintenance completed. Pilot training fordaily inspections will be given by Club flight instructors during the process ofa student’s licence training and /or as part of any type conversion trainingprocess.

3.4 AUTHORITY OF MAINTENANCE PERSONNEL

(1) The Chief Engineer of the Club's approved maintenance organisation, whenauthorised to carry out any maintenance work on a Club aeroplane, assumesresponsibility in the rectification of any defect or fault affecting airworthiness.

(2) Notwithstanding the above, the Chief Engineer is not authorised to carry outany major repairs or replacements found to be necessary during a workshopinspection without prior consultation with the Chief Pilot and specific authorityfrom the Club's management to perform that maintenance

3.5 FUEL DOCUMENTATION

(1) On completion of the refuelling operation, the pilot in command is to ensurethat the amount of fuel recorded by the refueller agrees with the amountdispensed into the aircraft's tanks and that this amount is entered in the 'TOTAL

LITRES' column on the Fuel Sheet.

(2) Before commencing each flight or flight segment, the pilot in command shallbe personally responsible for checking the amount of any fuel dispensed intothe aeroplane and for verifying, by means of fuel gauges and, if possible,visually or by dip stick, that the total fuel on board is sufficient for theproposed flight in accordance with the Club's "Fuel Policy" stated in sub-section 6.17 of Section A6, this Part.

(3) On operations away from the Club's home base, any fuel dockets obtainedshall be retained with the Passenger Manifest and, on return, these dockets willbe processed in accordance with the Club's office procedure along with any fueldockets obtained locally.


© AEROSERVICE 2000


3.6 FUEL USAGE RECORDS

(1) For the purposes of verifying the flight planning fuel consumption rate for eachaeroplane operated by the Club, the pilot in command shall ensure that all fueladded to the aeroplane's tanks and the fuel remaining at the end of a flight isrecorded on the current Fuel Sheet for that aeroplane.

(2) All completed Fuel Sheets shall be retained for a minimum of twelve months.

(3) A copy of the Club Fuel Sheet is shown at Appendix 1 to this Section.

3.7 PERSONS PERMITTED TO TAXI AIRCRAFT

(1) Club aircraft shall not be taxied at any time by a person other than:

(a) a licensed pilot whose licence or log book is endorsed for that particulartype of aeroplane;

(b) the holder of a Certificate of Approval issued in accordance with CAO20.22.

(2) The persons referred to in (1)(a) and (b) above must also be approved by theClub for the purpose.

WARNING

Any unauthorised taxiing of aircraft may invalidate the Club's aviation hull andliability insurances.

3.8 PERSONS PERMITTED TO OPERATE CONTROLS

(1) The flight controls of a Club aeroplane may only be manipulated by;

(a) a person holding an appropriate pilot licence and ratings who is assignedfor duty on board that aeroplane; or

(b) a pilot assigned for instruction in the aircraft; or

(c) a person who is authorised by CASA.

WARNING

Any unauthorised operating of aircraft controls may invalidate the Club'saviation hull and liability insurances.




3.9 PROCEDURE IN THE EVENT OF UNSERVICEABILITY AWAY FROM HOME BASE

L (1) Except as provided for at sub-section 3.3(3) of this Section, the pilot incommand must notify the HAAMC or, if unavailable, the Chief Engineer of theClub's approved maintenance organisation concerning any unserviceabilityaway from home base. An entry detailing the unserviceability shall be madein Part 2 of the Maintenance Release in accordance with sub-section 3.2 ofthis Section.

L (2) The HAAMC or Chief Engineer may, depending on a diagnosis of the defector fault and local availability of an appropriately licensed aircraft maintenanceengineer, authorise the pilot to carry out certain checks or arrange for alicensed aircraft maintenance engineer to proceed to the site.

L (3) In certain cases the Chief Engineer may, after consultation with the HAAMC,seek approval from the CASA to ferry the aircraft back to home base ifprovision for a ferry operation is not made in the Minimum Equipment List forthat aeroplane, for the particular unserviceability.

(4) Under no circumstances shall a Club pilot depart on a flight for the purpose ofa ferrying a multi-engine aeroplane to another aerodrome if that flight willrequire flying the aeroplane with one engine inoperative.

3.10 MAINTENANCE AND SERVICING OF AIRCRAFT AND AIRCRAFT COMPONENTS

(1) Maintenance Control and Maintenance Organisations

(a) Where the Registered Operator of an aircraft operated by the Club isheld by an entity other than the Club, the Management Committee of theClub shall ensure that an agreement is in place detailing theresponsibilities of each party for the airworthiness control of that aircraft.A copy of this agreement is shown at Appendix 4 to this Section.

(b) As circumstances dictate, the Management Committee shall ensure thatsuitably approved and qualified organisations and engineers carry outand certify scheduled and unscheduled maintenance, checks, defectrectification and compliance with airworthiness directives on Cluboperated aircraft and on emergency equipment used in Club operations.

(c) Before an organisation carries out maintenance on Club operatedaircraft, including individuals on an ad hoc basis, the Club shall obtainfrom prospective organisations or individual engineers, copies ofcertificates of approval, aircraft maintenance engineer licences,categories, ratings, specific aircraft training, approvals of engineersemployed and details of equipment to be used. The Manager shall retaincopies of the above documents for the organisations or engineersperforming maintenance on Club operated aircraft. ....





(2) Responsibilities of Personnel

L (a) The HAAMC shall be responsible for:

(i) ensuring that all organisations directed to perform maintenancehave appropriately licensed personnel to certify for the completionof all maintenance and that procedures for training of maintenancepersonnel are in place for aircraft added to the Club's fleet and forrecurrent training;

L (ii) ensuring that maintenance personnel have access to current issuesof the relevant technical data. Where organisations do not haveaccess to the relevant data, the HAAMC shall request that therequired data is obtained;

(iii) ensuring that Registered Operators for Club operated aeroplanesare made aware of the requirement to notify the Chief Pilot of allAirworthiness Directives, Service Bulletins, Service Letters ormaintenance directions issued by a recognised Authority ormanufacturer to the Registered Operator. This notification shall bemade on the Registered Operator’s Maintenance Advisory Notice.Refer to Page 2 of Appendix 4;

(iv) directing maintenance organisations to perform scheduled andunscheduled maintenance, defect rectification and ServiceBulletins, Service Letters or maintenance directions requirementsusing the Club’s Maintenance Advisory Notice. A copy of this Noticeis shown at Appendix 3 to this Section;

(v) aircraft maintenance planning and control in conjunction with theChief Engineer of the Club’s maintenance organisation;

(vi) Airworthiness Directives, Service Bulletin, Service Letters ormaintenance directions review in consultation with the Certificate ofRegistration holder and ensuring compliance where required;

(vii) ensuring that aircraft log books, engine log books, propeller logbooks, history cards, and other maintenance certificationdocuments are preserved, protected from deterioration or alterationand retained for the applicable period as detailed in CAO 100.5.5.2.

(viii) ensuring that all pilots are proficient in carrying out the DailyInspection, tie-down procedures and pilot maintenance for theaircraft they are required to fly and organising training if and whenrequired. ....





(2) Responsibilities of Personnel

(b) The Chief Engineer of the nominated Maintenance Organisation(s) whichperform maintenance on Club operated aircraft are responsible for:

(i) ensuring that all organisations directed to perform maintenancehave appropriately licensed personnel to certify for the completionof all maintenance;

(ii) ensuring that organisations directed to perform maintenance haveaccess to current issues of the relevant technical data;

(iii) maintenance release issue;

(iv) when requested by the Registered Operators of Club operatedaeroplanes, maintaining a system for each Club aircraft to list andmonitor aircraft components with a time/life or reconditioning period,applicable Airworthiness Directives, Service Bulletin, ServiceLetters, maintenance directions, high time inspections and specialinspections. For aircraft maintained in accordance with acomputerised system of maintenance, this will be as detailed in theapplicable Instruction Manual;

(v) aircraft technical data, maintenance direction, service bulletin andservice letter reviews in consultation with the Chief Pilot;

(vi) airworthiness directives, maintenance direction, service bulletin andservice letter compliance including notification and endorsingmaintenance release with urgent compliance requirements;

L (vii) actioning Maintenance Advisory Notices issued by the Club’sHAAMC;

(viii) weight control of Club aeroplanes;

(ix) permissible unserviceability applications;

(x) applications for Special Flight Permits;

(xi) applications for exemptions and/or variations to the CAR's;

(xii) defect investigation;

(xiii) defect report submission;

(xiv) transfer of aircraft records to new Registered Operators;

(xv) training of Club pilots in CAR Schedule 8 maintenance, as required.....





(3) Repairs, Modifications, Replacements or Adjustments

L (a) The Management Committee of the Club shall require the nominatedmaintenance organisations to carry out repairs, modifications,replacements or adjustments on Club operated aircraft or aircraftcomponents strictly in accordance with an approved maintenanceschedule and that maintenance required to be performed in accordancewith that schedule is carried out when required by that schedule.

L (b) The nominated maintenance organisation shall utilise the aircraft andcomponent manufacturers' maintenance and overhaul manuals andsupplementary service information, as applicable unless any of thoseschedules have been found to be deficient, in which case, the Club shallrequire that the chief engineer request approval for alternatemaintenance schedule(s) from the Civil Aviation Safety Authority.Repairs or modifications may also be carried out in accordance withdrawings, engineering notes or other design documents approved by theCivil Aviation Safety Authority or an approved person;

(c) All replacement components must be serviceable and except wherepreviously installed as a result of modifications, shall:

(i) be identical with components they replace, or

(ii) be specified in the applicable aircraft or component manufacturer'sparts catalogue as a superseding or alternative part; and

(iii) supplied under the cover of applicable documentation provided bya recognised authority or manufacturer.

(d) Special and/or Supplementary Inspections shall be carried out inaccordance with the aircraft manufacturer's instructions. Specialinspections may also be promulgated by the Civil Aviation SafetyAuthority or by the Club and approved by the Civil Aviation SafetyAuthority. These inspections shall be carried out in accordance with theprocedures specified by the applicable document. Where theseprocedures differ from a procedure contained in the manufacturer'smanual, the procedure required by the CASA approved specialinspection must be observed.

....





(4) Airworthiness Directives, Maintenance Directions and Service Bulletins

L (a) The CEO shall ensure that aircraft Certificates of Airworthiness andCertificates of Registration are current. The HAAMC shall ensure that anyAirworthiness Directives or maintenance direction issued by CASA or otherrecognised Authority, or notification of suspension or cancellation of aCertificate of Registration for an aircraft for which the Club is the holder orupon notification from the Registered Operator, is passed to the ChiefEngineer of the Club’s maintenance organisations and to flight crew whoare rostered to fly that particular aircraft;

L (b) The HAAMC shall review each issue of Airworthiness Directives, ServiceBulletins, Service Letters or similar documents for applicability to aircraftoperated by the Club and take appropriate action to ensure that allapplicable requirements are complied with within the stated compliancelimits.

L (c) The HAAMC will discuss with the Chief Engineer any AirworthinessDirectives, Service Bulletin, Service Letter or similar documentconcerned with maintenance as soon as possible after receipt andensure arrangements are made for compliance. Should such documenthave a recurring requirement, the HAAMC shall ensure that thisrequirement is added to the aircraft's maintenance record system.

(5) Defect Reporting and Investigation

(a) Where the pilot in command of a Club aeroplane becomes aware of theexistence of a major defect or that the aeroplane has suffered majordamage he/she shall enter details of the defect or damage on Part 2 ofthe Maintenance Release and advise the Chief Pilot of the endorsementon the Maintenance Release prior to further flight;

L (b) The HAAMC shall inform the Chief Engineer and, if applicable, theaircraft’s Registered Operator, details of the defect or damage. TheHead of Aircraft Maintenance shall liaise with the Chief Engineer of theClub’s approved maintenance organisation to determine rectificationaction;

L (c) Where a defect is considered to be a major defect (CAR 51A), theHAAMC shall submit a report immediately to the CASA with respect tothe defect;

....





(5) Defect Reporting and Investigation (Cont’d)

L (d) In the course of rectification of a defect referred to in (c) above or

defects as defined in CARs 51 or 52, the HAAMC shall request the Chief

Engineer to conduct an investigation to determine the cause of that

defect and to complete and furnish a Defect Report Form to the CASA

within 2 working days of the discovery of the defect. A copy shall also be

furnished to the HAAMC;

(e) Details of the Defect Report Form (Form 404), reporting guidelines and

methods of reporting in relation to defects are detailed in CAAP 51-1(1).

(6) Modifications

If any modification or repair to a Club aircraft or aircraft component is required

and for which an approval has not been granted by CASA or an approved

person, or a change of maintenance schedule or changes to an existing

maintenance schedule are required, an application for approval for that

modification, repair or change shall be made to CASA by the Chief Engineer of

the Club's maintenance organisation on the request of the Club.

(7) Daily Inspections

(a) Daily inspections shall be carried out in accordance with the Daily

Inspection Schedule specified in the relevant aircraft log book. Persons

authorised to certify for the completion of a daily inspection on Club

aircraft are Club instructors or the pilot in command who is the holder of

private or higher category pilot licence endorsed for the aircraft type or

group, or a LAME licensed in either the airframe or engine category;

(b) Completion of daily inspections shall be certified by the person carrying

out the inspection in the space provided in Part 3 of the current

Maintenance Release for the particular aircraft.

L (c) Where the daily inspection is conducted in the absence of the pilot in

command, the person conducting the daily inspection shall inform the

pilot in command of its completion and of any defects found.

....





(8) Fuel and Oil

(a) The pilot in command is personally responsible for ensuring that all fluidshe/she causes to be delivered into the aircraft comply with the requiredstandards and specifications;

(b) Pilots must consult the individual aircraft Flight Manual for details of theapproved grades and specifications of fuels and oils applicable to thataircraft;

(c) Club pilots may assume that any aviation fuels, engine lubricating oilsand other aircraft fluids delivered into an aircraft by any accredited oilCompany representative will comply with the specified standards inevery respect.

(9) Weight Control

L (a) The HAAMC and the Chief Engineer shall ensure that all periodicreweigh requirements are complied with in accordance with CAO 100.7;

(b) The Chief Engineer shall ensure that all weight and balance variationsresulting from modifications, repairs or aircraft configuration changes arereflected in the aircraft weight and balance record and aircraft loadsystem and such alterations are completed by the holder of anappropriate CASA weight control authority.

(c) The Club shall issue and the pilots shall only use loading data which hasbeen issued by an approved weight control officer for Club aeroplanes.

L (d) Duplicate copies of all approved loading data issued for Club aeroplanesshall be kept by the HAAMC in a safe place on the ground.

(10) Portable Equipment

Club pilots may use portable airborne radio equipment in Club aeroplanesprovided;

(a) that equipment does not interfere with installed equipment; and

(b) any portable radio communication equipment intended to be used forcommunication with ATS or other aircraft shall be of a type approved byCASA and is connected to an approved external antenna system; and

(c) a portable navigation system which requires an external antenna is onlyconnected to an external antenna approved by CASA.





(11) Amendment Service

L The Manager shall ensure that an amendment service for Airworthiness

Directives, aircraft Flight Manuals, Maintenance Manuals and associated

Service Directives, Letters or Bulletins are in place with the appropriate

aircraft manufacturer.

(12) Calibration Of Tools And Equipment

The maintenance organisation shall only use tools, equipment and test

apparatus, whose accuracy is essential to the work performed, that have been

inspected, tested and calibrated in accordance with, and at the periods

specified in, the Calibration Register maintained by maintenance organisation.

The Chief Engineer of the maintenance organisation shall be responsible for

ensuring that all tools and equipment in use are within the specified calibration

period and meet the required standards.

3.11 CARRIAGE OF PERSONS IN SEATS AT WHICH DUAL CONTROLS ARE FITTED

(1) The second control seat of an Club aeroplane fitted with dual controls may

only be occupied by a person holding an appropriate pilot licence and ratings,

a pilot assigned for instruction in the aeroplane or a person who is authorised

under CAO 20.16.3, sub-section 11.1.

(2) For single pilot aeroplanes a person who is authorised under CAO 20.16.3,

sub-section 11.1 may, with the approval of the pilot in command, occupy a

control seat provided that person is given adequate instructions as amplified

in sub-section 4.10(4) of Section A4.

(3) If rudder pedals are fitted to the second control seat position, the passenger

is to be briefed thoroughly on the need to keep his/her feet off the pedals,

unless the pedals are of the type which can be set flush with the floor, in which

case the pilot in command is to ensure they are set flush with the floor for

such flights.


© AEROSERVICE 2000


3.12 STARTING AND GROUND OPERATIONS OF ENGINES

(1) An engine of a Club aeroplane shall only be started and operated by a Club

pilot endorsed on the aircraft type or by a Licensed Aircraft Maintenance

Engineer who is the holder of a Certificate of Approval issued in accordance

with CAO 20.22. Except as detailed in 3.12(3) below, a person referred to

above shall remain at the controls of the aeroplane while the engine is

running.

(2) No person shall be permitted to handle the propeller of any Club aircraft for the

purposes of starting the engine unless he/she has been instructed in and is fully

conversant with the correct hand starting procedure for that aircraft.

(3) The pilot in command of a Club operated aeroplane which requires an

operating crew of only one pilot, may manipulate the propeller of that

aeroplane for the purpose of starting an engine but only when:

(a) the pilot has been instructed in and is fully conversant with the correct

hand starting procedure for that aeroplane; and

(b) another pilot endorsed on the aircraft type or the holder of a Certificate

of Approval issued in accordance with CAO 20.22 is on board the aircraft

to operate the engine controls and brakes; or

(c) if the assistance as required by (b) above is not readily available;

(i) adequate provision is made to prevent the aircraft moving forward;

and

(ii) no person is aboard that aircraft.

(4) The engine of a Club aeroplane shall not be started for any purpose within the

distances below;

(a) 5 m of any sealed building;

(b) 8 m of an unsealed building or an aircraft; or

(c) 15 m of an exposed public area.

WARNING

Any unauthorised operation of aircraft controls may invalidate the Club's

aviation hull and liability insurances.




3.13 GROUND OPERATION OF WEATHER RADAR

(1) The weather radar installed in a Club aeroplane shall not be operated in otherthan the STBY mode on the ground unless the area that will be scanned is clearof the following objects to a distance of 37 metres;

(a) aircraft being fuelled or defuelled;

(b) fuel tankers, fuel tanks or fuel storage areas;

(c) persons or cargo;

(d) any aircraft of aircraft hangar.

3.14 AIRCRAFT COMPONENT CONTROL

L (1) The Club’s maintenance organisation shall normally control the purchase,repair and storage of components intended for use in Club aeroplanes inaccordance with that organisation’s Procedures Manual. Where the Clubpurchases or stores aircraft components, the control of those componentsshall be in accordance with the following procedures.

(2) Aircraft components held by the Club for use in Club aeroplanes shall bestored in a secure area free from contamination with protection from sunlight,excessive heat and moisture. The components shall be held in physicallyseparate areas according to the following;

(a) Inspection Area - components received and held by the Club before thecompletion of a conformity inspection;

(b) Bonded Area - following completion of the conformity inspection,components held for distribution to the Club’s maintenance organisationfor installation in Club aeroplanes. Components which have a shelf lifeshall be segregated from components not subject to a shelf life within thebonded area;

(c) Rejected Area - components which have failed the conformity inspectionto be marked 'UNSERVICEABLE' and segregated for return to the supplier;

(d) Unserviceable Area - components which have been removed from aaeroplane and which are suitable for overhaul. These components shallbe tagged 'UNSERVICEABLE' and physically segregated from allserviceable stock until overhauled and made serviceable. ...




3.14 AIRCRAFT COMPONENT CONTROL

(3) All inward components shall be subject to the following procedures;

(a) components shall only be purchased from organisations which canprovide documentation tracing the history of the component back to themanufacturer;

(b) components are to be segregated from existing stock until inspection fortransport damage, identification and documentation check for conformityand authenticity is carried out;

(c) all components will be entered in the Club’s Component Receipt andIssue Register and will be marked with the corresponding ComponentReceipt Number. Components will then be placed into the Bonded Area;

(d) a "SERVICEABLE" tag shall filled in and attached to the component.

(4) Component Receipt and Issue Register

A number will be allocated to the entry which will indicate the progressivenumber for that inward consignment for that calendar year, the month ofreceipt and the last two digits of the year ie. 243/10/98. The register will alsorecord;

(a) date of receipt;

(b) part number;(c) description (including serial number if applicable)(d) quantity;(e) supplier;(f) documentation - release note(g) freight Company and docket number;(h) shelf life (if applicable);

On issue of the component;

L (i) date of issue to the aircraft;

(j) intended aircraft for installation; and

(k) remarks.

L A copy of a Component Receipt and Issue Register is shown at Appendix 5to this Section.

(5) Unserviceable components removed from a aeroplane which cannot beoverhauled, shall be rendered unfit for further use and destroyed.




3.15 PORTABLE ELECTRONIC DEVICE

(1) No passenger carried aboard a Club aircraft shall operate any portable

electronic device except devices listed in (2) below and medical equipment

such as heart pacemakers and hearing aids which may be used without

restriction.

(2) Non transmitting devices may be used except during climb or descent or when

the pilot in command requests that the device be switched off. Examples of

these devices are listed below:

(a) calculators; and

(b) laptop computers, provided they comply with Part 15 of the US FCC

rules.

(3) Hand held communication radios used by operating crew for communication

with ground personnel may be used in flight provided the equipment is tested

for interference with the aircraft’s radios before flight. Other transmitting type

devices such as those listed below shall not be used at any time during flight.

(a) computerised video games;

(b) walkie talkies;

(c) CB radios;

(d) radio controlled toys.

(4) Mobile phones shall not be used at any time during flight except in an

emergency or where other means of communication are not available or have

failed.

3.16 EMERGENCY EQUIPMENT RECORD

L The HAAMC shall maintain a list of Club survival equipment and the overhaul/expiry

information for that equipment. A copy of Emergency Equipment Inspection Record

is shown as Appendix 6 to this Section.




3.17 GPS DATABASE UPDATING

L (1) GPS data bases in Club operated aeroplanes may be updated by a Club pilot

in accordance with the following;

(a) where the database is updated by inserting a data card into the facia of

the GPS receiver - by a Club pilot who has received training conducted

by the Chief Pilot in the use of the particular type of GPS equipment;

(b) where the database is updated by loading data from a disk or a PCMCIA

card or via the Internet - by a Club pilot who has received training

conducted by the Chief Pilot in the use of the particular type of GPS

equipment and has received training in the method of updating. This

training shall be recorded in the pilot’s records.

(2) The pilot shall make an endorsement on the Maintenance Release indicating

the current cycle and expiry date in accordance with sub-section 3.1 of this

Part.GG

© AEROSERVICE 2000

08/00 THE REDCLIFFE AERO CLUB Section A3AIRCRAFT ADMINISTRATION Appendix 1

Page 1FUEL SHEET

DATE REGO METER READINGS

(FROM KEY)

TOTAL

LITRES

CASH

RECEIVED

RECEIPT

NUMBER

AIRCRAFT

TACHO

CONSUMPTION

HOURLY/RATE

INIT

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. . . . . . . . . . TOTAL

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AIRCRAFT ADMINISTRATION Appendix 2

Page 1

SCHEDULE 8 Paragraph 42ZC (4)

MAINTENANCE THAT MAY BE CARRIED OUT ON A CLASS B AIRCRAFT

BY A PILOT ENTITLED TO DO SO UNDER SUBREGULATION 42ZC (4)

1. Removal or installation of landing gear tyres, but only if the removal or installation does not

involve the complete jacking of the aircraft.

2. Repair of pneumatic tubes of landing gear tyres.

3. Servicing of landing gear wheel bearings.

4. Replacement of defective safety wiring or split pins, but not including wiring or pins in control

systems.

5. Removal or refitting of a door, but only if:

(a) no disassembly of the primary structure or operating system of the aircraft is involved; and

(b) if the aircraft is to be operated with the door removed - the aircraft has a Flight Manual and

the manual indicates that the aircraft may be operated with the door removed.

6. Replacement of side windows in an unpressurised aircraft.

7. Replacement of seats, but only if the replacement does not involve disassembly of any part of the

primary structure of the aircraft.

8. Repairs to the upholstery or decorative furnishings of the interior of the cabin or cockpit.

9. Replacement of seat belts or harnesses.

10. Replacement or repair of signs and markings.

11. Replacement of bulbs, reflectors, glasses, lenses or lights.

12. Replacement, cleaning, or setting gaps of, spark plugs.

13. Replacement of batteries.

14. Changing oil filters or air filters.

15. Changing or replenishing engine oil or fuel.

16. Lubrication not requiring disassembly or requiring only the removal of non-structural parts, or of

cover plates, cowlings and fairings.

17. Replenishment of hydraulic fluid.

18. Application of preservative or protective materials, but only if no disassembly of the primary

structure or operating system of the aircraft is involved.

19. Removal or replacement of equipment used for agricultural purposes.

20. Removal or replacement of glider tow hooks

21. Carrying out of an inspection under regulation 42G of a flight control system that has been

assembled, adjusted, repaired, modified or replaced.

22. Carrying out of a daily inspection of an aircraft.



Page 1


MAINTENANCE ADVISORY NOTICE

L From: The Redcliffe Aero Club Registered Operator:

To: Attention:

Sign: Date:

The maintenance detailed in the attached document identified as:

is due on VH Aircraft Type Serial No. and is to be

completed by Date Aircraft Hours Aircraft Cycles .

For Operator Use Only

VH will be available at on and is required for return to

operation at on .

Acknowledgment of receipt of the Maintenance Advisory Notice, acceptance of the maintenance

detailed and confirmation of completion of the maintenance shall be forwarded to:

Chief Pilot The Redcliffe Aero Club Phone: 07 3203 1777

ACCEPTANCE

Maintenance Advisory Notice received and request for maintenance detailed accepted by:

Name For and on behalf of

Sign Date

COMPLETION

Maintenance completed and aircraft returned to service on at am/pm.


Sign Date



Page 2


L REGISTERED OPERATOR’S ADVISORY NOTICE

From:(Registered Operator)

To: The Redcliffe Aero Club Attention: Chief Pilot

Sign: Date:

The maintenance detailed in the attached document identified as:

is due on VH Aircraft Type Serial No.

ACKNOWLEDGMENT

Acknowledgment of receipt of the Registered Operator’s Advisory Notice, acceptance of themaintenance detailed and confirmation of completion of the maintenance shall be forwarded to:

Registered Operator: Phone:

ACCEPTANCEMaintenance Advisory Notice received and request for maintenance has been made to:


Sign Date

COMPLETIONThe above maintenance has been completed.


Sign Date


01/05 THE REDCLIFFE AERO CLUB Section A3L AIRCRAFT ADMINISTRATION Appendix 4


CROSS-HIRE AGREEMENT - AIRWORTHINESS CONTROL OF AIRCRAFT VH-

This document confirms the contractual arrangements in place, clarifying a division of responsibilities for

the airworthiness control for aircraft:

Type Serial number Reg’d VH-

during the Cross-Hire period; From / / To / /

L The Registered Operator is:

and the aircraft will be operated under Air Operators Certificate # by

(1) The monitoring and control of all life limited components and special inspection requirements for this

aircraft are provided by;

Name: Company

Procedures / Document

Frequency

(2) Airworthiness control and maintenance documentation provision and arrangements for provision

of the associated revision service from the applicable approved data source are provided by;

Name: Company


Frequency

page 1 of 3


10/00 THE REDCLIFFE AERO CLUB Section A3L AIRCRAFT ADMINISTRATION Appendix 4

Page 2



(3) Incoming applicable technical data, bulletins and the like, for this aircraft shall be assessed for

possible implementation to this aircraft by;

Name: Company


Frequency

(4) Compliance requirements from A.D.’s, Aircraft and Component Manufacturers’ maintenance

requirements, service bulletins etc. applicable to this aircraft are determined by;

Name: Company


Frequency

(5) The person responsible for providing and maintaining the technical library, amendment status, and

timely provision of relevant service information for this aircraft is;

Name: Company


Frequency

(6) The person who controls airworthiness liaison for this aircraft with the appointed approved aircraft

maintainer is;

Name: Company


Frequency

page 2 of 3





(7) The person who controls the servicing, installation / removal, and maintenance and upkeep of the

role equipment fitted to this aircraft is;

Name: Company


Frequency

(8) The person who is responsible for the training of operations staff who are involved in the

airworthiness facets of the above-mentioned role equipment handling, installation / removal

procedures and activities is;

Name: Company


Frequency

(9) The agreed procedures between the parties for the reporting of flying hours, and data transfer for

pertinent operational data such as trend monitoring and condition reporting, defect control and

required maintenance are as follows;

Parties to this agreement, - agreement is hereby acknowledged by the signing of this form,:

Signed Name on behalf of;




page 3 of 3 Rev. - Revision 1, 17 Jan, 2005


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L GENERAL Appendix 6

Page 1




SECTION A4

PASSENGER AND FREIGHT ADMINISTRATION

SUB-SECTION PAGE

4.1 PASSENGER DOCUMENTATION A4-3

4.2 FREIGHT DOCUMENTATION A4-3

4.3 STANDARD PASSENGER WEIGHTS A4-4

4.4 USE OF SEAT BELTS A4-4

4.5 CARRIAGE OF MINORS A4-4

4.6 LOADING PROCEDURES AND CARGO RESTRAINT A4-5

4.7 GROUND FACILITIES A4-8

4.8 FREIGHT HANDLING EQUIPMENT Reserved

4.9 FREIGHT RECEIPT AND DISPATCH A4-8

4.10 BRIEFING OF PASSENGERS A4-8

4.11 SMOKING A4-11

4.12 CARRIAGE OF DANGEROUS CARGO A4-11

4.13 CARRIAGE OF ANIMALS A4-12

....




SECTION A4

PASSENGER AND FREIGHT ADMINISTRATION

SUB-SECTION PAGE

4.14 MOVEMENT AND SURVEILLANCE OF PASSENGERS ON

TARMAC AREAS A4-13

4.15 INTOXICATED AND OFFENSIVE PASSENGERS A4-13

4.16 PASSENGER COMFORT A4-14

APPENDIXES

1. PASSENGER MANIFEST AND FLIGHT RECORD

2. CONSIGNMENT NOTE

L

L

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© AEROSERVICE 2000

08/00 PASSENGER AND FREIGHT ADMINISTRATION A4-3

4.1 PASSENGER DOCUMENTATION

(1) For all passenger charter flights a Passenger and Cargo Manifest shall becompiled. A copy of the Manifest shall be left at the place of departure in thecustody of a Club representative or other responsible person.

(2) If a passenger embarks at an intermediate stopping place, a new Manifestmust be compiled and a copy left at that place except where that particularchange had been notated on the copy of the Manifest left at the initialaerodrome of departure.

(3) Where a new Manifest has to be compiled at a remote location or at a landingarea where there is no Club agent, it is the pilot's responsibility to fill out theManifest and leave a copy with a responsible person or in a prominentpredetermined position.

(4) Where student pilots are carried as passengers on training flights, the namesof the student shall be entered in the Flight Authorisation;

(5) All completed Manifests shall be retained for a minimum of 3 months.

(6) A copy of the Club's Passenger and Cargo Manifest is shown at Appendix 1to this Section.

4.2 FREIGHT DOCUMENTATION

(1) Before any cargo, other than passenger baggage carried on the sameaeroplane as the passenger, is accepted for carriage by air, a consignor must;

(a) complete a Consignment Note;

(b) describe the contents of the cargo; and

(c) sign and date that Consignment Note.

A copy of the Club's Consignment Note is shown at Appendix 2 to thisSection.

(2) It is the responsibility of the pilot in command to ensure that the total weightof each consignment is recorded on applicable Consignment Note and thetotal weight of all Consignment Notes is transferred to the Manifest for theparticular flight.

(3) A freight manifest supplied by a freight forwarder may contain a signeddeclaration that the cargo does not contain dangerous goods and shoulddescribe the contents and the weight of the cargo. If this is not provided, aConsignment Note shall be completed.


© AEROSERVICE 2000


4.3 STANDARD PASSENGER WEIGHTS

(1) Load calculations for all Club operated aircraft will be made using actual

weights for all passengers and baggage carried.

(2) It is the responsibility of the pilot in command not to exceed the

maximum weights specified for the aircraft in use

4.4 USE OF SEAT BELTS

(1) The pilot in command and pilots under instruction shall wear a seat belt

properly fastened at all times during flight.

(2) The pilot in command shall ensure all occupants occupy a seat with the seat

back adjusted to the upright position and are wearing a seat belt at the

following times:

(a) during take-off and landing;

(b) whenever the aircraft is flying at a height less than 1000 feet above the

terrain;

(c) during an instrument approach;

(d) during turbulent conditions; and

(e) at such other times when the pilot in command considers that seat belts

should be worn in the interests of safety.

(3) The pilot in command shall ensure that each seat belt is adjusted to fit the

wearer without slack, and in the case of infants and children, the seat belts

are fitted in the manner prescribed at sub-section 4.5 this Section.

4.5 CARRIAGE OF MINORS

(1) Two children may occupy one seat (other than a control seat or a seat

adjacent to an emergency exit) if seated side by side provided their combined

weight does not exceed 77 kg. The seat belt shall be adjusted to secure both

children at all times when seat belts are required to be worn.

....




4.5 CARRIAGE OF MINORS

(2) One infant or child may carried in excess to the maximum number of

passengers in a Club operated aircraft which has seating capacity of between

two and six passenger seats.

NOTE: A person who has reached 13 years of age may not occupy the same

seat with another person.

L (3) An infant may be carried in the arms or on the lap of an adult passenger and

in such cases, the name of the infant shall be bracketed on the Passenger

Manifest with the name of the person carrying or nursing the infant. The infant

shall be restrained by a “supplementary loop belt” attached to the adult’s seat

belt. Refer to CAAP 235-2.

L (4) An infant may be carried in a bassinette, or a car type infant seat provided the

seat complies with either FAA TSO C100b, Australian design standard AS

1754, ECE Reg 44 or is acceptable to the UK CAA, providing the unit is

installed in a manner consistent with the seat's design criteria.

The infant seat should be;

(a) used and serviced in accordance with the manufacturers instructions;

(b) not be located in the row forward or aft of an emergency exit;

(c) not block access and passageways to any emergency exit.

The condition of these seats is the responsibility of the owner of the seat.

4.6 LOADING PROCEDURES AND CARGO RESTRAINT

(1) Loading Procedures

(a) The calculation of weights for all passengers and cargo carried in

aeroplanes shall be in accordance with sub-section 4.3, this Section. All

weights shall be recorded before the aircraft is loaded.

(b) Cargo, except for the pilot’s briefcase, shall not be carried on an

unoccupied control seat. The seat belt on an unoccupied control seat

shall be secured to prevent interference with the flight controls.

(c) A passenger, acceptable to the pilot in command, may occupy a control

seat of a Club operated aeroplane provided that person is given adequate

instructions as amplified in sub-section 4.10(3) of Section A4. ....





(1) Loading Procedures (Cont’d)

(d) Passenger seats may be removed to permit the carriage of cargo where:

(i) the removal of passenger seats for this purpose is authorised by the

Flight Manual when relevant instructions must be strictly adhered

to; or

(ii) an approved loading system for that aircraft in the freighter

configuration is used.

(e) It is a specific requirement of the Club that whilst passengers are being

processed prior to loading, the pilot in command identifies, as far as it is

possible to do so without causing unnecessary embarrassment, any

persons who may be handicapped and ensures that such persons are

seated in the aircraft where they will not unduly obstruct or hinder access

to emergency exits by other persons on the aircraft.

(f) Cargo shall only be carried in a place or compartment where a placard

stating the loading limitations is affixed and legible.

(g) The pilot in command shall ensure that loose articles including catering

items are correctly restrained to prevent movement and that all

passageways and exits are kept free of obstructions at all times the

aeroplane is in flight.

(h) Passengers and cargo shall not be loaded or un-loaded while an engine

in a Club aeroplane is running.

(2) Cargo Restraint

(a) The pilot in command shall ensure that all cargo carried is properly

restrained by the use of approved tie-down straps and/or approved cargo

nets, depending on the location and nature of the load, using normal tie-

down points provided in the aeroplane and seat or seat belt anchorages,

as applicable, in a manner which prevents any article from moving under

the maximum accelerations to be expected in flight and in an emergency

landing or ditching.

(b) The strength of the restraint equipment shall be suitable to restrain the

cargo under the maximum load factors for flight, ground, or emergency

landing conditions to which the particular aeroplane is certified. ....





(2) Cargo Restraint (Cont’d)

L (c) All equipment restraint equipment shall be labelled with the name of the

approved manufacturer and include maximum load capacity. The pilot

in command shall ensure that restraint equipment used has been

designed for that particular purpose.

(d) Cargo carried on unoccupied seats, shall be restrained in accordance

with the following requirements;

(i) the cargo and restraint does not interfere with any flight or other

controls or carried on a seat adjacent to an emergency exit;

(ii) The total weight of such cargo carried shall not exceed 77 kg per

seat and such weight is evenly distributed over the squab;

(iii) the cargo shall be restrained by an approved cargo restraint so as

not to move under 9G force forwards and 3G upwards and

sideways. Seat belts shall not be used for this purpose unless as

part of an approved restraint;

(iv) handles or carry straps on baggage shall not be used as the means

of restraint of an article;

(v) notwithstanding the above, passenger personal effects may be

carried aboard providing that the passenger is briefed to restrain the

item or items, during take-offs and landings, and in flight in

turbulence.

(3) Weight and Balance Requirements

(a) The pilot in command of a aeroplane operated by the Club, before any

flight, shall ensure:

(i) The aeroplane is loaded within the prescribed centre of gravity

limits as determined by the current approved loading system

specified in the aircraft Flight Manual for that aeroplane;

(ii) The maximum take-off weight of that aeroplane or the gross weight

for take-off, whichever is the lesser, is not exceeded; and

(iii) The centre of gravity of that aeroplane will not move outside the

approved range at any time whilst in flight. ....



06/08 PASSENGER AND FREIGHT ADMINISTRATION A4-7a


(3) Weight and Balance Requirements (Cont’d)

(b) The individual aeroplane loading and aircraft Flight Manual limitations

are to be complied with at all times.

(4) Weight and Performance Limitations

(a) When determining the aeroplane's load, the pilot in command shall take

into account all factors that may affect adversely that aeroplane's

performance such as altitude AMSL, temperature, humidity and other

local factors likely to have a detrimental effect on its performance.

(b) For relevant performance data refer to the appropriate chart/tables in the

individual aircraft Flight Manual.

L (5) Load Rejection Policy

(a) Where due to operational requirements it is necessary to off-load

payload to carry additional fuel, the priority of off-loading shall be in the

order of cargo, baggage, passengers.

(b) Passengers must be advised when off-loading baggage so they may

have the option of not travelling without their baggage as some

passengers may have medication or similar in their baggage that they

cannot do without.




06/08 PASSENGER AND FREIGHT ADMINISTRATION A4-7b





4.7 GROUND FACILITIES

(1) Scales for the weighing of crew and equipment are located at the Club’s mainoperating base.

L (2) A set of scales is to be carried in the aircraft whenever crew and equipmentare to be loaded at locations where weighing facilities may not be readilyavailable to the pilot and the applicable weights have not been notified to theClub in advance. Bathroom type scales are considered suitable for thispurpose.

L (3) The Chief Pilot shall ensure that passenger and cargo weighing scales arecalibrated at 12 monthly intervals by weighing a known weight. The scalesshall be adjusted if required. The person conducting the check shall place asticker on the scales showing the date for the next calibration check.

4.9 FREIGHT RECEIPT AND DISPATCH

L (1) The Club requires that a person who consigns any cargo for carriage on boardan aircraft must make a signed declaration. This shall be completed on theClub's Consignment Note as detailed in sub-section 4.2(1) above.

(2) Any consignment of cargo for which the shipper has declared on theConsignment Note that the shipment contains dangerous goods shall not beaccepted for carriage on board a Club aeroplane.

(3) A consignment of freight need not be weighed if the consignor submits acertified statement as to the weight of that consignment and the pilot incommand is completely satisfied that the weights provided by the consignorare reliable.

L (4) For the guidance of all operational personnel, a list of possible hazardousarticles is shown in Appendix 3 "Hidden Dangerous Goods", to Section A8.

4.10 BRIEFING OF PASSENGERS

L (1) While intending passengers are being briefed in accordance with thissub-section, the pilot in command of the aircraft or the authorised groundcrew conducting the briefing shall ensure that:

L (a) each person has been warned against the carriage of Dangerous Goodsother than as provided for in sub-section 8.3(1)(a) of Section A8 and tothe notice displayed on Club premises.

(b) those persons who may have been involved in underwater divingactivities have been made aware of the limitations applicable to flyingafter underwater diving as detailed at sub-section 1.21 of Section A1.

....





(2) Before engine start, the pilot in command shall ensure that all hand baggage

and other loose articles are safely stowed and that all passengers are clearly

and audibly briefed in relation to the following:

(a) name of the crew;

(b) the use of seat belts as specified at sub-sections 4.4 and 4.5 of this

Section and the appropriate method of fastening and adjustment. Also

recommend that passengers keep their seat belt fastened at all time in

case of unexpected turbulence;

(c) the no smoking requirements specified at sub-section 4.11;

(d) the aircraft's oxygen system, where applicable;

(e) location and method of operation of emergency exits including doors and

other openings which may be used for that purpose;

(f) where applicable, the location of the first aid kit, survival kit, life jackets

or life rafts;

(g) The restrictions on the operation of personal electronic devices in flight.

(h) location and operation of ventilation and climate controls;

(i) general details of flight time, en route weather and other pertinent

information;

(j) if applicable, the location of the passenger briefing card and an outline

of the information contained on that card.

L (3) When a passenger is authorised to occupy a control seat, that person shall be

additionally briefed before flight in respect of the following:

(a) to not move the seat from its lateral position;

(b) to keep the safety harness or seat belt securely fastened at all times;

(c) to not touch or obstruct the flight controls, or knobs, switches, etc. on the

instrument panel;

(d) the location and operation of the emergency exit(s); and

(e) the need for that person to remain alert for any instructions that may be

specifically directed to him/her during flight. ....





L (4) When a sick, injured or otherwise handicapped person is being carried, thatperson shall be given individual briefing before flight, appropriate to his/herneeds, in respect of the following:

(a) all relevant aspects of the general passenger briefing; and

(b) the procedures to be followed in the event of an emergency evacuationof the aircraft including the emergency exit to be used and the mostappropriate manner of assisting that person from the aircraft.

L (5) When engaging in overwater flights requiring the carriage of life jackets inaccordance with CAO 20.11, the pilot in command shall ensure that allpassengers have been orally briefed before flight on their location and use.The person conducting the briefing shall use a demonstration life jacket toshow:

(a) correct method of donning and securing the tapes with specialinstructions relating to any children aboard the aircraft;

(b) method of actuating the compressed air cylinder. Impress on passengersthat life jackets are not to be inflated whilst the wearer is still inside theaircraft;

(c) method of inflating by use of the mouthpiece should further inflation berequired or the air cylinder fail to operate;

(d) method of actuating the locater light; and

(e) purpose and use of the whistle.

L (6) When life rafts are carried, a passenger briefing shall be conducted beforeflight and shall include the following:

(a) that the life rafts are to be moved outside the aircraft and the painter linesecured to a hardpoint in or on the aircraft before inflation;

(b) that, before inflation, the life raft should be in an upright position andmoved as far as possible from the aircraft;

(c) method of inflation;

(d) location of the knife to be used for cutting the painter line.

L (7) Where a person, other than the pilot in command, conducts a briefing ofpassengers, that person shall inform the pilot in command before departure,that the briefing has been conducted.




4.11 SMOKING

(1) The pilot in command shall ensure that smoking in the aircraft by passengersis prohibited at the following times:

(a) during take-off and landing, whenever the aeroplane is operating at lessthan 1000 feet above ground level and whilst the aircraft is being refuelled;

(b) during such periods as are specified in the Flight Manual for that aircraft;

(c) during the use of any specialised equipment which may specify thatsmoking is prohibited, e.g. oxygen; and

(d) during such other periods when the pilot in command considers thatsmoking should be prohibited in the interests of safety.

(2) Every effort should be made to dissuade passengers from smoking if there isany likelihood of causing respiratory problems or discomfort to any otherperson on board.

4.12 CARRIAGE OF DANGEROUS CARGO

L Refer to Section A8 for the administration of dangerous goods.

4.13 CARRIAGE OF ANIMALS

(1) Except as specified in (2) and (3) below, animals may be carried in Clubaircraft in accordance with the following conditions;

(a) the animal is carried in an approved container which is carried in acompartment other than a passenger cabin;

(b) the container shall be constructed so as to prevent the escape of theanimal, water or waste from the container;

(c) the container must be of a size to prevent the movement of the animalor the animal is restrained from movement within the container;

(d) the carriage of an animal must not adversely affect the safety of theaeroplane or persons carried on board

(2) Animals other than a dog accompanying a visually or hearing impairedperson as a guide or assistant shall not be carried in the passengercompartment of an aircraft whenever that compartment is occupied by apassenger.




4.13 CARRIAGE OF ANIMALS

(3) A guide/assistant dog may, subject to prior arrangement, accompany its

master in the passenger compartment of an aircraft provided:

(a) the dog is placed on a moisture absorbent mat as near to the person as

practicable; and

(b) is restrained in a way that will prevent the dog from moving from the mat.

(4) Club personnel are reminded that the carriage of certain animals may be

subject to the stock disease laws of the States or Territories in which the

animals are carried. For further information refer to the Department of

Agriculture in the appropriate State or Territory.

4.14 MOVEMENT AND SURVEILLANCE OF PASSENGERS ON TARMAC AREAS

(1) Club pilots and operational support personnel are collectively and individually

responsible for ensuring that:

(a) No unauthorised person is allowed to trespass, remain, operate a

vehicle, or bring any animal or bird onto an area of an aerodrome

controlled by the Club;

(b) Minors are not allowed anywhere on the tarmac area unless they are

under the control of the person directly responsible for their welfare;

(c) Persons, other than Club personnel are not allowed to move without a

responsible escort in the vicinity of any aircraft which has its engine(s)

operating or is about to start;

(d) All passengers have been briefed on the appropriate method of

proceeding to and from an aircraft; and

(e) All passengers have been briefed on the requirements not to smoke on

a defined tarmac area, within a placarded "No Smoking" area or within

15 meters of the aircraft; and

(f) Passengers are always escorted to and from the aircraft.




4.15 INTOXICATED AND OFFENSIVE PASSENGERS

(1) The pilot in command of the aircraft, in accordance with the authority which

is vested in him/her under Regulation 309 of the Civil Aviation Regulations,

may refuse to carry any intoxicated or other passenger who, because of that

person's general behaviour, is regarded by the pilot to be offensive or a likely

threat to the safety of the aircraft or of the other persons on board.

(2) Provoking the passenger should be avoided at all costs, and expressions such

as 'intoxicated' or 'under the influence of alcohol/drugs' should not be used

when discussing refusal or off loading as this places the onus of proof on the

Club and may even result in later legal action. A discreet "In my judgement

as pilot in command of the aircraft you do not appear to be in a suitable state

of health to fly today" may be all that is needed to deal effectively with the

problem.

4.16 PASSENGER COMFORT

(1) Passenger comfort must be of prime concern to crew members and ground

staff alike and a high standard of courtesy should be demonstrated at all

times. The pilot should ensure that the passengers know the location and

operation of ventilation and climate controls and are made aware of any

special features designed for their individual comfort.

(2) When sick, injured or handicapped persons are being carried, the pilot in

command shall take all reasonable precautions to minimise discomfort to other

occupants.

(3) Passenger comfort is also complimentary to safety and in order to maintain

maximum passenger comfort and confidence in the air, pilots should take all

reasonable steps to avoid

- areas of atmospheric turbulence;

- sudden or violent flight manoeuvres;

- steep turns; and

- descending at more than 500 feet per minute.GG

© AEROSERVICE 2000

08/00 THE REDCLIFFE AERO CLUB Section A4PASSENGER AND FREIGHT ADMINISTRATION Appendix 1

Page 1

PASSENGER MANIFEST AND FLIGHT RECORD

Call Sign DATEHIRER/NAME . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

VH- ADDRESS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

DeparturePoint

DepartureTime . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Post Code . . . . . . . . . . . . . . PH . . . . . . . . . . . . . . . . . . . . . . .

ArrivalPoint

ArrivalTime

PASSENGER NAMES

1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Fuel atDep/Pt

Freight atDep/Pt

2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

CombinedPax/Wts

T.O.W.At Dep/Pt

5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

6 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

Pilot flighttime:

8 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

PILOT NAME

Remarks: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

© AEROSERVICE 2000

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PASSENGER AND FREIGHT ADMINISTRATION Appendix 2

Page 1


© AEROSERVICE 2000


SECTION A5

EMERGENCY PROCEDURES

SUB-SECTION PAGE

5.1 DECLARATION OF EMERGENCY A5-3

5.2 EMERGENCY CHANGE OF ALTITUDE A5-3

5.3 COMMUNICATION FAILURE A5-4

5.4 NAVAID FAILURE A5-4

5.5 DIVERSIONS DUE TO WEATHER A5-4

5.6 ABNORMAL LANDINGS A5-5

5.7 EMERGENCIES WITH STUDENT OR INEXPERIENCED PILOTS A5-9

5.8 FLIGHT IN ABNORMAL METEOROLOGICAL CONDITIONS A5-10

5.9 CONTINUED FLIGHT IN ABNORMAL CONDITIONS A5-12

5.10 PASSENGER CONTROL IN ABNORMAL SITUATIONS A5-13

5.11 ACTION IN THE EVENT OF UNLAWFUL INTERFERENCE Reserved

5.12 ACTION IN THE EVENT OF BEING FORCED DOWN OR

UNABLE TO TAKE-OFF IN A REMOTE AREA A5-14

5.13 BIRD STRIKES AND AVOIDANCE A5-14

5.14 CLUB FLIGHT FOLLOWING PROCEDURES A5-15

....


© AEROSERVICE 2000


SECTION A5


SUB-SECTION PAGE

5.15 SERIOUS ILLNESS ON BOARD A5-16

5.16 USE OF FIRE EXTINGUISHERS A5-16

5.17 DITCHING A5-16

5.18 FUEL SPILLS A5-17

5.19 PRESSURISATION FAILURE Reserved

APPENDIXES

1. WIND - SWELL - DITCHING HEADING



04/04 EMERGENCY PROCEDURES A5-3

5.1 DECLARATION OF EMERGENCY

(1) Should the aircraft be in grave and imminent danger, e.g. engine failure, fire

or serious airframe malfunction, the early transmission of a distress message

(MAYDAY - see AIP/ERSA) and selection of transponder code 7700 will

ensure maximum assistance with minimum delay.

(2) An urgency message (PAN - see AIP/ERSA) is the appropriate transmission

should the safety of a person be involved, or the aircraft be experiencing

performance or navigational difficulties and, as with the distress message,

early transmission and transponder selection to 7700 is essential for maximum

assistance.

(3) Club pilots are expected to be fully conversant with AIP/ERSA so that the

appropriate procedure may be instantly initiated should an emergency or

abnormal situation arise or be observed in flight, or if unable to comply with

the Rules of the Air or ATC requirements.

L (4) An AIR SAFETY ACCIDENT OR INCIDENT REPORT shall be furnished by the pilot

in command within 2 working days of an occurrence in accordance with the

requirements set down at sub-section 6.12 of Section A6..

5.2 EMERGENCY CHANGE OF ALTITUDE

(1) The conditions which may require the initiation of an emergency descent to a

lower altitude include

- navigational difficulties;

- engine malfunction;

- build up of smoke in the cabin;

- fire;

(2) Any necessity for an emergency descent shall be immediately reported to ATS

so that separation can be arranged, but if this is not possible, turn away from

the area of known traffic to avoid conflict with other aircraft and transmit the

appropriate signal as prescribed in AIP/ERSA.


© AEROSERVICE 2000


5.3 COMMUNICATION FAILURE

Where a total communication failure occurs in flight, the pilot in command shall

follow the COM failure procedures in AIP/ERSA.

5.4 NAVAID FAILURE

Where total communication and navaid failure occur in flight, the pilot in command

shall follow the COM and NAVAID failure procedures in AIP/ERSA.

5.5 DIVERSIONS DUE TO WEATHER

(1) Flight in IMC

If a successful approach and landing at the destination aerodrome appears

marginal due to weather, the pilot in command shall make an allowance for

diversion to an alternate in accordance with the fuel reserves detailed in sub-

section 6.17(4)(c) of Section A6.

(2) Flight in VMC

(a) Club aircraft shall not commence a VFR flight unless current

meteorological reports and forecasts show that the weather conditions

en route and at the destination are such that the flight can be conducted

under the visual flight rules.

(b) If weather conditions begin to deteriorate, the pilot in command must

carefully monitor the changes and plan possible alternative action. Pilots

are referred to CAR 171(2) and are reminded that where an aircraft

cannot be flown in accordance with the Visual Flight Rules, the pilot in

command shall comply with the Instrument Flight Rules, provided the

pilot is rated and the aircraft has the appropriate equipment for operating

under the IFR, or land at the nearest suitable aerodrome.

(c) The pilot in command is at all times responsible for the safety and

security of the aircraft including persons on board and is expected to

take whatever action is deemed necessary having regard for the existing

and all other possible circumstances.

....


© AEROSERVICE 2000


5.5 DIVERSIONS DUE TO WEATHER

(3) Unscheduled Landing

(a) If an unscheduled landing due to weather cannot be avoided, it should be

carried out while sufficient fuel remains to permit a normal landing.

(b) The pilot in command, when determining the suitability of an aerodrome

or ALA for an unscheduled landing, should consider, in addition to the

operational requirements, the availability of accommodation, transport,

communications and, if required, facilities for the refuelling and servicing

of the aircraft.

(c) Notification and a full report will be made to the Chief Pilot within 24

hours of the occurrence.

5.6 ABNORMAL LANDINGS

(1) Club pilots should always be aware of the proximity of aerodromes suitable for

an emergency diversion. The suitability of an aerodrome for a diversion

following an inflight emergency will depend on the aircraft type, the type of

emergency and the availability of rescue and fire fighting services.

(2) If a decision is made to divert to aerodrome following an in flight emergency,

the pilot in command shall consider all the relevant factors. Refer to sub-

section 2.4 of Section B2, Part A, for the factors to be considered if a decision

is made to continue to an aerodrome other than the nearest aerodrome.

(3) Following an abnormal landing, the pilot in command shall consider whether

the aeroplane should be stopped on the runway or clear of the runway. In the

event of the possibility of fire, turn the aeroplane to place the emergency exit

and/or door on the upwind side of the aeroplane. Refer to sub-section 5.10(2)

for the Evacuation Procedure.

(4) The checks detailed below in this sub-section are to be used where

applicable checks are not published in the Pilot’s Operating Handbook

for the aeroplane.

....


© AEROSERVICE 2000



(4) Abnormal Landings Immediately After Take-off - Multi-engine Aeroplanes

If an engine failure or fire occurs after take-off, Club pilots shall;

(a) complete the Engine Failure after Take-off Checklist;

(b) climb to a safe altitude;

(c) advise ATS with intentions;

(d) if possible, remain clear of cloud;

(e) brief the passengers as detailed in sub-section 5.10;

(f) carry out the checklist for a single-engine landing;

(g) select a suitable runway. If the performance of the aeroplane is such thata landing on the departure runway may not be possible, select a suitablearea inside the aerodrome if possible, i.e. taxiway, runway strip, disusedrunway etc.;

(h) do not reduce the airspeed below VXSE to "stretch" the distance the aeroplaneis capable of covering;

(i) only extend the gear when a safe landing is assured. Be prepared toaccept a gear up landing.

(5) Engine Failure in Flight - Multi-engine Aeroplanes

If sufficient height and airspeed is available at the first sign of an in flightengine failure, the pilot in command shall complete the following checksbefore securing the affected engine;

(a) Mixture control - FULL RICH

(b) Check fuel pressure; if not normal; fuel boost pump - ON, checkpressure;

(c) Fuel selector - SELECT to another fuel tank containing fuel;

(d) Magneto switch - SELECT Right to Left to Both. If the engine respondswith a change of switch selection, leave the magneto switch in thatposition;

(e) Oil pressure and temperature - NORMAL;

(f) If the engine does not respond, complete the applicable engine securingchecklist; and

(g) brief the passengers as detailed in sub-section 5.10(1). ....


© AEROSERVICE 2000



(6) Complete Loss of Engine Power after Take-off

Following a complete loss of engine power after take-off where sufficient

height and airspeed are not available to complete any troubleshooting

checks, Club pilots shall adopt the following procedure;

(a) Lower the nose immediately to maintain airspeed above stall speed;

(b) Fuel selectors - OFF;

(c) Battery, alternator and magneto switches - OFF

(d) Mixture control - IDLE CUTOFF BOTH;

(e) Warn forward facing passengers to adopt a brace position;

(f) Keep straight ahead. Chance direction only to avoid obstacles. Use

rudder only. Keep wings level;

(g) Always maintain enough airspeed to ensure full control of aircraft to

point of touch-down. Coarse use of ailerons near the stall airspeeds

precipitates wing dropping. It is better to fly an aircraft with complete loss

of engine power safely to a controlled crash landing straight ahead, than

to make an attempt to turn back to the aerodrome.


....





(7) Complete Loss of Engine Power in Flight

Following a complete loss of engine power in flight where sufficient height and

airspeed are available to complete any troubleshooting checks, Club pilots

shall adopt the following procedure;

(a) Mixture control - Both FULL RICH

(b) Check fuel pressure; if not normal; fuel boost pump - Both ON, check

pressure;

(c) Fuel selector - SELECT each side to another fuel tank containing fuel;

(d) Magneto switch - SELECT each to Right to Left to Both. If an engine

responds with a change of switch selection, leave the magneto switch in

that position;

(e) Oil pressure and temperature - Both NORMAL;

(f) If the engine(s) do not respond, complete the applicable engine securing

checklist from the Emergency Procedures Section of the aircraft Flight

Manual or Pilot's Operating Handbook, as applicable to the aeroplane in

use; and

(g) Reduce the airspeed to the appropriate glide speed. If in IMC turn

towards lower terrain. When in VMC select a suitable landing area.

(h) Squawk 7700 and transmit a "Mayday" call giving position and

intentions;

(I) Brief the passengers as detailed in sub-section 5.10(1).

(j) Activate the ELT, if possible.

(k) Carryout a forced landing





5.7 EMERGENCIES WITH STUDENT OR INEXPERIENCED PILOTS

(1) Should an in-flight emergency arise during a dual instructional flight, the

instructor must take over control of the aircraft. Control is deemed to have

changed upon the instructor stating "taking over" and on receiving an audible

"handing over" from the pilot under training.

(2) Before authorising a solo flight, the authorising instructor should be satisfied

that the student pilot has sufficient knowledge to handle any emergency or

adverse flight condition that may occur. The trainee must also be familiar with

the procedures outlined at sub-sections 5.1 through 5.6, this Section.

(3) The flight must not be authorised unless the requirements of the last

preceding paragraph can be satisfied beyond reasonable doubt.

(4) When information is received of an emergency involving a student or

inexperienced pilot operating Club aircraft, the Chief Pilot or CFI or other most

senior staff member on duty should be immediately notified.

L (5) The Civil Aviation Safety Authority must also be notified of any condition which

may result in an emergency situation.

(6) If an emergency could involve damage to aircraft or injury to crew or members

of the public, the relevant fire, police and ambulance authorities shall be

alerted.

(7) In the case of a landing problem involving student pilots or trainees flying solo,

the Chief Pilot or CFI or other most senior staff member on duty should be

immediately notified. If an attempt to render assistance by radio is thought

helpful, it should be borne in mind that the inexperienced pilot is under

considerable strain, and all directions should therefore be simple, clearly

worded and definitely and authoritatively given.



© AEROSERVICE 2000


5.8 FLIGHT IN ABNORMAL METEOROLOGICAL CONDITIONS

(1) The abnormal meteorological conditions likely to be encountered by Club

pilots are thunderstorms and cyclones The weather conditions likely to be

associated with thunderstorms and cyclones are heavy rain, strong winds and

squalls, hail, severe turbulence, icing, lightning, low visibility and low cloud

and, for water float plane operations, rough surface conditions.

(2) When thunderstorms are forecast, Club pilots shall ensure that all Club

aeroplanes on the ground are either hangared or, if a hangar is not available,

the aeroplane is securely tied down into the anticipated wind with all control

locks in place.

(3) If a severe thunderstorm warning or cyclone warning is current, Club

aeroplanes shall either be placed in a hangar or if the aircraft cannot be

adequately protected, consideration should be given in consultation with the

Chief Pilot to flying the aircraft to a safer location.

(4) When flight planning to an area where a cyclone watch is current and, Club

pilots should consider planning for an alternate landing point outside the watch

area, as the cloud, wind strength and direction may change considerably. If

required by a charter client to remain for a period of time at an aerodrome where

a cyclone watch is current, the pilot in command shall remain vigilant for any

deterioration in the weather. The pilot shall remain in contact with the client

in case an earlier departure is required.

(5) Thunderstorms and Airborne Weather Radar

(a) The weather radar system is designed for weather avoidance and will

not be used to penetrate thunderstorms unless an emergency exists and

no safer course is available. If thunderstorm conditions are observed or

forecast, it is the responsibility of the pilot in command to carefully

analyse the situation and, if possible, detour the area. Such deviations

are desirable even though the flight may have to be refuelled enroute.

Weather radar must never be used as a collision avoidance or ground

proximity warning device

(b) Only Club aircraft with operative radar may enter cloud areas where

thunderstorm activity is being experienced. If the radar is inoperative or

not fitted the pilot must operate in VMC in any thunderstorm area. ....


© AEROSERVICE 2000


5.8 FLIGHT IN ABNORMAL METEOROLOGICAL CONDITIONS

(5) Thunderstorms and Airborne Weather Radar (Cont'd)

(c) If the weather radar is not fitted or fails enroute, it is the responsibility of

the pilot in command to determine if a thunderstorm area can be

navigated with safety and reasonable comfort to passengers. He/she

should review latest available weather reports and consider all

information regarding thunderstorm conditions. The pilot should, when

possible, plan routes which will avoid forecast thunderstorm areas. While

enroute he/she should avoid thunderstorms visually.

(6) Echo Avoidance Policy

(a) When the pilot interprets thunderstorm conditions exist from the radar

returns, it is desirable that the area be detoured. An early decision to

divert around a thunderstorm will need a relatively small heading

change and result in minimum distance added to the flight.

(b) When timely evasive action is not possible, the following shall apply:

(i) When using the shorter range setting to circumnavigate echoes,

monitor the longer ranges frequently to determine the extent of the

area and to watch for additional developments;

(ii) Navigable corridors between echoes should be reasonably straight

and at least 20 nm wide;

(iii) Avoid flying under a cumulonimbus overhang when possible;

(iv) Avoid steep rainfall gradients by 10 nm or more;

(v) Increase the distance in (iv) by 100% or more for echoes which are

rapidly increasing in size or intensity, changing shape rapidly, exhibit

hooks, fingers, scalloped edges or other forms of protrusion.

(c) When taking-off in thunderstorm areas, the radar should be operated on

the ground using some upward antenna tilt to determine the best

possible climbout path. During ground operation the radar must be left

in the standby position until the aircraft is clear of all large reflective

objects by 30 metres. Take-offs and landings shall not be attempted

unless the clearance criteria detailed above is available.


© AEROSERVICE 2000


5.9 CONTINUING FLIGHT IN ABNORMAL CONDITIONS

(1) Abnormal Engine or System Operations

(a) Except as detailed in (b) below, Club pilots shall land at the nearest

suitable aerodrome/ALA and shall not continue flight with any abnormal

engine or system operation.

(b) Following an engine or system malfunction in flight, the continuation to

an aerodrome other than the nearest suitable aerodrome shall be at the

discretion of the pilot in command after consideration of all relevant

factors including;

(i) the nature of the malfunction and the possible mechanical

difficulties which may be encountered if the flight is continued;

(ii) availability of an malfunctioning engine or system for use;

(iii) the altitude, aircraft weight and usable fuel at the time of failure;

(iv) distance to be flown and the type of terrain enroute;

(v) relative characteristics of the aerodromes available for a landing;

(vi) weather conditions enroute and at the available aerodromes;

(vii) familiarity of the pilot with the aerodromes suitable for use.

(c) When an engine fails or is shut down in flight or the aircraft suffers a

system malfunction in flight, the pilot in command shall notify the nearest

ATS unit as soon as possible giving the relevant information and the

intentions of the pilot in command.

(2) Meteorological Conditions

Club pilots shall divert and land at the nearest suitable aerodrome/ALA or

return to the departure point if meteorological conditions are encountered

which are not suitable for continued flight.



© AEROSERVICE 2000


5.10 PASSENGER CONTROL IN ABNORMAL SITUATIONS

(1) Briefing

During an emergency the pilot in command shall remain in control and ensurethat all passengers are seated with seat belts correctly fastened and will briefthe passengers on;

(a) nature of emergency;

(b) approximate flight time remaining and destination (if applicable);

(c) type of landing anticipated;

(d) removal and securing of sharp objects;

(e) brace position to be adopted;

(f) use of emergency exits, if an abnormal landing is envisaged.

(2) Evacuation Procedure

When the aircraft has come to rest after an emergency landing, the pilot incommand shall;

(a) determine which evacuation exits to be used considering;

(i) amount of damage;

(ii) aircraft attitude;

(iii) water level (if ditching);

(iv) fire danger;

(v) propeller rotation.

(b) when a decision has been made on the exits to be used, the pilot incommand shall;

(i) open emergency exit/door;

(ii) direct and assist passengers with evacuation;

(iii) ensure all passengers have left the aircraft;

(iv) leave the aircraft;

(v) inflate life jacket (if ditching);

(vi) assemble passengers in a group take command;

(vii) activate ELT.




5.12 ACTION IN THE EVENT OF BEING FORCED DOWN OR UNABLE TO TAKE-OFF

IN A REMOTE AREA

(1) If a Club aeroplane operating in a designated remote area is forced to make

an unscheduled landing for reasons of weather or mechanical failure, or is

similarly unable to take-off, radio communication should immediately be

established with ATS, the Club or other aircraft to obtain the necessary

assistance.

(2) If communications cannot be established, the pilot should activate the

aeroplane's emergency locater transmitter, either at the nominated Sartime or

after allowing time for the Club to realise the aeroplane is overdue.

(3) The pilot and all other persons on board must stay with the aeroplane until

located or, if weather is the cause of the grounding, until conditions have

sufficiently improved to permit a safe continuation of the flight. The

aeroplane's survival equipment and survival handbook should be utilised as

necessary in the meantime.

(4) It is permissible for the pilot or other person to leave the grounded aeroplane

to seek assistance only if it is absolutely certain that a town, settlement, road

or homestead is within reasonable distance, but notes should be left and a

trail made which can be followed by a land party.

5.13 BIRD STRIKES AND BIRD AVOIDANCE

(1) Birds pose a major problem to aircraft in parts of the country at various times

of the year. Often at early morning and late afternoon they will follow defined

paths when foraging for food or may be forced to shelter due to climatic

conditions.

(2) Where possible avoid areas of high bird concentration. Little can be done to

make the aircraft more obvious except for displaying all possible lights.

(3) While most birds will dive to avoid an aircraft, their behaviour is unpredictable

and unless ground staff are available to disperse them, it may be prudent to

delay arrival or departure until they have moved on.

L (4) Any bird strike must be reported to ATSB using the Aviation Bird & Animal

Strike Notification form.


© AEROSERVICE 2000


5.14 CLUB FLIGHT FOLLOWING PROCEDURES

(1) If a Club aeroplane is conducting a flight without submitting flight notificationto Airservices, the following procedures shall be adopted to enable the Club tomaintain an effective flight following for Club aeroplanes. Club pilots shall notifythe Club office of the following details;

(a) Registration;

(b) Details of flight;

(c) Names of persons on board; and

(d) Nominated Sartime.

(2) Club pilots are to contact the Club by phone before the expiry of theirnominated Sartime.

(3) If a pilot has not contacted the Club by his/her nominated Sartime or upon thenotification of the overdue arrival of any Club aeroplane, the followingprocedures shall be instigated.

The Club through the Chief Pilot or delegate shall;

(a) Try to contact the aeroplane concerned. (i.e. radio, phone, another Clubaircraft or client representative);

(b) Obtain from the Club's client, the probable area of operations and lastknown position and the number of persons on board;

(c) Notify the following information to Australian Search and Rescue (AMSA)telephone 1800 815 257, Fax 1800 62 2153:

(i) the registration of the aeroplane that is missing

(ii) last known position and notified intentions.

(4) On finding the missing aeroplane, the following procedures shall be instigatedby the Chief Pilot in conjunction with the AMSA RCC:

(a) Ascertain from the AMSA the number of survivors and the best possiblemethod of rescue, if required;

(b) Obtain the position of the aeroplane and of the nearest landing area;

(c) Instigate planning and logistics for a possible retrieval aircraft if required.....


© AEROSERVICE 2000


5.15 SERIOUS ILLNESS ON BOARD

In the event of serious illness occurring on board a Club aeroplane, take whataction is necessary to stabilise the patient. Advise ATS and request priorityhandling if considered necessary. Request medical advice or assistance andconsider diverting to a suitable aerodrome where medical facilities are available.

5.16 USE OF FIRE EXTINGUISHERS

Should the use of fire extinguishers be necessary in the cabin, move thepassengers as far away as possible and be alert for the possibility of toxic fumesfrom the burning material or effects of the extinguishing agent.

5.17 DITCHING

The following procedures shall be adopted by Club pilots if specific ditchingprocedures are not incorporated in the aircraft Flight Manual for the aeroplane inuse.

(1) Sea Evaluation

"SWELLS" which are almost never absent, wind or not, are caused by a distantdisturbance. The major swell is almost always accompanied by at least oneminor swell moving from a different direction. "WAVES" are caused by thelocal wind. They move in the same direction as the wind. Periodically theswells and waves are in the opposite phase, with the crests of one filling thetroughs of the other, giving a resultant smoother surface. Such areas are thebest areas for ditching. Refer to Appendix 1, this Section

The opposite applies when in phase. Wind velocity can be assessed byobserving the WIND LANES and WHITE CAPS.

White caps move forward with the wind, but are overtaken by the waves,giving the illusion that the foam is sliding backwards.

WIND TABLE

FEW WHITE CRESTS 10 - 20 Knots

MANY WHITE CRESTS 20 - 30 Knots

STREAKS OF FOAM 30 - 40 Knots

SPRAY FROM WAVES 40 - 50 Knots ....


© AEROSERVICE 2000


5.17 DITCHING

(2) Heading Selection

The objective is to select a landing direction that will result in the minimum

relative speed between the aircraft and the swell system. The best heading is

parallel to the major swell and down the minor swell, making the greatest use

of the headwind component. Both major and minor swells travel from 20 to 45

knots and must be considered when ditching.

The final heading will depend on the velocity of the wind versus the velocity

and height of the minor swell. If the minor swell is considered too formidable,

and downwind component too great, select heading parallel to the minor swell

and down the major swell.

Landing down swell reduces relative touch-down speed by the speed of the

swell.

(3) Ditching Technique

At 2000 feet;

- Observe the major swell;

- Note the wind speed and direction;

- Take up a general ditch heading along the swell into any existing

headwind component.

At 200 feet

- Adjust heading to correct for possible change in observed major and/or

minor swell system;

- Ditch into wind if wind speed is above 30 knots.

Descend to and hold 10 feet

- Look ahead for relative smooth area. Judging height above glassy water

is deceptive. Employ the IFR technique to alight

- Touch down on or just past the crest of the swell

- It may be possible to utilise ground effect to prolong touching down if the

aeroplane if any power is available.

....


© AEROSERVICE 2000


5.17 DITCHING

(4) Alighting - Visually

- After closing the throttles, rotate aircraft to a slightly higher attitude than

a normal landing attitude, and contact water with minimum speed and

rate of descent.

DO NOT STALL THE AIRCRAFT

(5) Impact

Be prepared for two or more impacts. Do not unfasten seat belts or move

around until it is quite sure the aircraft has stopped moving.

Due to slow speed characteristics of the most light aircraft, the aircraft will

ditch in a satisfactory manner and provide sufficient scope for evacuation of

the occupants. Reduce fuel to lowest practical minimum before landing. Empty

or nearly empty fuel tanks will provide additional buoyancy. Ensure sufficient

fuel is available for a power on landing

(6) Alighting IFR

(a) At night all bright internal lights should be switched off. Red lights are

more suitable to accustom eyes to darkness. Use "Map" lights set to Red

on the flight deck. Set cabin lights to "Dim" .

(b) Take up a ditch heading 90 deg. to the forecast surface wind obtained

from charts, ground station or prior briefing, unless the wind speed is

above 35 knots, then into wind heading.

(c) From 1,000 feet, adjust rate of descent to 100 - 200 FPM; IAS 10 - 15

knots above the stall with full flaps.

(d) Use the RH landing light only.

(e) This approach should be maintained until the aircraft makes contact with

the water or until visual contact is establish for ditching.

....


© AEROSERVICE 2000


5.17 DITCHING

(7) Cabin and Crew Preparation

The pilot in command must nominate those exits to be used.

WARNING

Do not open any exits in flight. Opening of any door before impact could

result in flooding.

(a) All exits should be used wherever practical when evacuating; down swell

exits may be the most suitable.

(b) The crew should ensure that exits are opened.

(c) State the particular exit each person should use unless circumstances

after impact dictate otherwise.

(d) Brief passengers to assist as required.

(e) Impact Position - Passengers to sit with arms cradled around knees,

head resting on arms, feet placed firmly on the floor.

(8) Stowage of Loose Equipment

All loose equipment such as hand luggage must. be stowed either under the

seats or preferably in the rear locker.

(9) Lighting

At night, after cabin prepared, switch off reading lighting and set cabin lighting

to "DIM" to accustom eyes to the darker conditions For ditching, use right.

hand landing fight only. Switch Beacon - OFF.

(10) Salvage

Items most useful will vary with circumstances but include, First Aid Kits,

torches, food, liquids, fire extinguishers, protective clothing, seat cushions

(lifebuoys),pillows and rugs. First Aid Kits are buoyant.

....


© AEROSERVICE 2000


5.17 DITCHING

(11) Life Rafts

(a) Exiting the Aircraft

In the event of a ditching the following is recommended as a guide for

actions to be taken assuming sufficient time is available.

Normally the main door will be used in a ditching. The emergency exit

over the wing may be used if the main door has jammed. It should be

above water level.

Before opening doors or removing the emergency exit remove the life

raft from its stowage and have it ready to be passed through the exit

onto the wing. Ensure the raft is not inflated while inside the aircraft.

When ready to evacuate the aircraft check outside for any damage which

could puncture the life raft.

Remove the emergency exit, if possible delegate an able bodied person

to proceed outside to assist the other occupants out and to help move

the life raft from the cabin to the outside.

Ensure the raft is deployed down wind to avoid fouling the aircraft and

is securely restrained to avoid drifting off in high wind or seas.

(b) To deploy the raft.

After it has been removed from the aircraft in its protective valise, locate

the D ring and inflation line. Secure the inflation line to the aircraft to

prevent losing the raft. Launch the valise into the water downwind of the

wing and give the line a sharp tug which will cause the raft to inflate.

Load the occupants and any supplies available. If a second raft is

carried launch the second raft in the same manner and if possible

secure the two rafts together for better visibility.

If the aeroplane remains afloat, try to stay in the area. However be

aware that the aeroplane may sink without warning.

....


© AEROSERVICE 2000


5.17 DITCHING

(11) Life Rafts

(b) To deploy the raft (Cont’d)

Activate survival beacons. Carefully read the instructions on the beacon

before using.

Follow the instructions in the survival kit. Be aware that exposure is a real

problem. Try to keep out of the sun and wind and keep as dry as possible.

Attend to the injured, maintain a lookout system, have flares or other

signalling devices ready. Collect any rain water available. Make best

use of all resources available.

(12) Water Survival Techniques - Life Raft Not Available.

If a ditching were to occur when life rafts are not available, the following water

survival techniques should be adopted.

Ensure life jackets correctly fitted and inflated after leaving the aircraft. Keep

together as individuals are more difficult to spot in the water.

Use the whistle and light to attract attention.

Do not fight the current if making for the shore. Swim at an angle across the

current and try to keep away from rocks may puncture the life jacket or may

cause injury.

If immersed in water for a considerable period try to reduce body heat loss by

adopting a foetal like position with the legs tucked up to the body.

If floating debris available use any item available to conserve strength.



© AEROSERVICE 2000


5.18 FUEL SPILLS

(1) If any fuel spill of a size which is likely to create a fire hazard occurs within 15

metres of a Club aeroplane or the refuelling equipment, the following action

is to be taken;

(a) the refuelling operation is to cease immediately;

(b) all passengers and other persons not assisting are moved at least 15

metres from the spilled fuel;

(c) the airport fire service or airport operator is to be notified;

(d) any vehicles or ground power units operating within 15 metres from the

spilled fuel are shut down;

(e) if possible, the aircraft is pushed by hand to a position at least 15 metres

from the spilled fuel.

(2) All available foam or CO2 fire extinguishers are moved to the area of the spill

before the removal of the fuel spill is commenced.

(3) Appropriate steps are used to remove the fuel spill without creating a fire

hazard.GG


EMERGENCY PROCEDURES Appendix 1

Page 1


© AEROSERVICE 2000


SECTION A6

FLIGHT CONDUCT

SUB-SECTION PAGE

6.1 FLIGHT AUTHORISATION A6-3

6.2 PREFLIGHT A6-3 6.3 REFUELLING PROCEDURES A6-5

6.4 LOW FLYING OPERATIONS A6-7

6.5 NIGHT FLYING OPERATIONS A6-8

6.6 MERCY FLIGHTS A6-8

6.7 INSTRUMENT APPROACH RECENCY A6-9

6.8 INSTRUMENT FLIGHT CONTINUATION TRAINING A6-9

6.9 FORMATION FLIGHT A6-10

6.10 TYPE ENDORSEMENT TRAINING A6-10

6.11 AEROBATICS A6-11

6.12 ACCIDENT AND INCIDENT REPORTING A6-11

6.13 OPERATIONS AT SPECIFIC LOCATIONS Reserved

6.14 SIMULATED ASYMMETRIC FLIGHT A6-13

6.15 HAND-OVER AND TAKE-OVER PROCEDURES A6-14

6.16 SIMULATION OF INSTRUMENT FLIGHT A6-14

6.17 PILOT BRIEFING AND FLIGHT PLANNING INSTRUCTIONS A6-15

6.18 MINIMUM PILOT EQUIPMENT AND DOCUMENTATIONTO BE CARRIED IN FLIGHT A6-18

6.19 PROCEDURES FOR STRAIGHT IN APPROACHES A6-19

....




SECTION A6

FLIGHT CONDUCT

SUB-SECTION PAGE

6.20 CREW CO-ORDINATION Reserved

6.21 USE OF CHECK LISTS A6-21

6.22 VISUAL AND INSTRUMENT DEPARTUREAND APPROACH PROCEDURES A6-21

6.23 OPERATIONS IN ENVIRONMENTAL EXTREMES A6-22

6.24 USE OF OXYGEN A6-22

6.25 DESCENT RATES WITH PASSENGERS ON BOARD A6-23

6.26 TURBULENCE PENETRATION A6-23

6.27 FLIGHT IN ICING CONDITIONS A6-24

6.28 NAVIGATION OF CLUB AIRCRAFT A6-24

6.29 MARSHALLING AND PARKING OF AIRCRAFT A6-25

6.30 OVERWATER OPERATIONS A6-26

6.31 AIREPS A6-27

6.32 DETERMINATION OF VISIBILITY AND CLOUD BASE A6-27

6.33 AIRCRAFT WEIGHT AND PERFORMANCE LIMITATIONS A6-27

6.34 OPERATIONAL PROCEDURES IN RELATION TO COMPUTERS A6-29

APPENDIXES

1. NAVIGATION LOG

2. CHECKLISTS FOR CLUB AEROPLANES

3. ACTION TO BE TAKEN IN THE EVENT OF AN ACCIDENT OR INCIDENT

L 4. PRECAUTIONS WHEN USING HIGH PRESSURE OXYGEN



03/06 FLIGHT CONDUCT A6-3

6.1 FLIGHT AUTHORISATION

(1) The Chief Pilot or delegated person shall be responsible for authorising allflights, other than flights for the purpose of flying training, with due regard tothe following:

(a) Maintenance status of the aircraft;

(b) Category or type of flight involved; and

(c) Pilot qualification requirements.

L (2) The means of flight authorisation shall be the entry on the amended rosterreferred to in sub-section 2.9(5) of Section A2. The conditions on authorisationin the absence of the Chief Pilot shall also be in accordance with thatsub-section.

(3) Maintenance flights for the purpose of testing a Club aircraft or an aircraftcomponent require the specific authorisation of the Chief Pilot.

(4) The pilot nominated as pilot in command on the Club roster is authorised tocarry out all necessary flight preparations and to perform the proposed flightprovided all relevant requirements are considered by him/her to besatisfactory for that flight.

(4) For authorisation of flights for the purpose of flying training, refer to sub-section 2.3, Part E.

6.2 PREFLIGHT

(1) Club operated aircraft shall not depart on a flight unless the pilot in commandhas ensured that:

(a) before the first flight of each day the aeroplane is operated, the followingis carried out;

(i) The Maintenance Release is checked for validity, any maintenancescheduled for the period of the proposed flight has been certified tohave been completed and any endorsement rendering theaeroplane unairworthy has been rectified and a certification hasbeen entered for its rectification;

(ii) A daily inspection, in accordance with the daily inspection scheduleapproved for the particular aircraft, is carried out and certified onthe Maintenance Release by either the pilot in command or by aperson approved under CAR 42ZC(4)(a).

(iii) A check for the presence of water from each fuel drain point iscarried out. ....




6.2 PREFLIGHT

(1) Club operated aircraft shall not depart on a flight unless ... (Cont'd)

(b) Prior to engine start, the pre-flight "walk around" inspection for thataircraft is fully carried out; and

(c) the following conditions have been met;

(i) the aeroplane is properly loaded;

(ii) sufficient fuel is aboard the aeroplane;

(iii) all external control surface locking devices have been removed bythe pilot in command;

(iv) all flights controls have been checked for full and free movementand if applicable, the second set of dual controls are not restrictedin any way;

(v) all external surfaces are completely free of frost and ice;

(vi) all fuel and oil tank caps are correctly fitted and secure and all fuelvents are free of obstructions; and

(vii) all doors, hatches and external fitments are secure for take-off.

(viii) all gyroscopic flight instruments are uncaged, tested and are functioningcorrectly.

(d) the nationality mark and registration mark is affixed and legible;

(e) prior to taxying on the manoeuvring area, the aeroplane's radios aretested for serviceability; and

(f) the applicable safety precautions, tests and checks, as applicable to theaeroplane type, are completed to ensure that the aeroplane is safe forflight;

(g) the compass correction card is installed, is legible and is within a threeyear period from the date on the card; and

(h) if the fuel tank gauge(s) are marked in fractions of tank capacity, aplacard showing the corrected readings at all major graduations and theungaugeable fuel quantity is installed and legible.

(2) Where any of the above inspections are conducted in the absence of the pilotin command, the person conducting the inspection shall inform the pilot incommand of its completion and of any defects found.

(3) If any inspection, test or check indicates a departure from permissible limitsor malfunctioning of any part of the aircraft, or in the equipment which isrequired to be used in flight, the pilot in command shall not commence thetake-off until that aircraft has been certified as serviceable by a personlicensed or approved for the purpose.




6.3 REFUELLING PROCEDURES

(1) General

Except as otherwise provided for in this sub-section, flight crew members andany operational support personnel who may be delegated to carry out,supervise or assist with refuelling or defuelling operations shall at all timescomply with the following requirements;

(a) no passengers shall be permitted to board or to remain on board theaeroplane during any refuelling operations;

(b) the aeroplane's engine is stopped with ignition OFF, external power isnot connected or dis-connected and no maintenance is conducted duringthe refuelling;

(c) two 4.5 Kg CO2 fire extinguishers or other types as approved by theCASA, shall be positioned between 6 and 15 meters of the aeroplane;

(d) except when draining fuel samples or transferring fuel between tanksusing the aircraft’s internal fuel transfer system, an aircraft and refuellingequipment shall be positioned at least 5m from a sealed building, 6mfrom other stationary aircraft, 9m from an unsealed building and 15metres from an exposed public area. The aircraft shall be positioned forrapid removal in the case of fire with the appropriate means available.Refuelling is not permitted in a hangar;;

(e) "NO SMOKING" signs shall be displayed and the limits of the no smokingarea shall be at least 15 meters.

(f) the fuel stock is checked for colour, clarity and freedom from dirt and/orvisible water by swirling a sample of the fuel in a circling motion so thatany sediment, etc. will collect in the centre bottom of the glass container.Water detecting paste shall be used for testing AVGAS for the presenceof water. If no water is detected the paste should be proven by theaddition of water or saliva to the surface of the paste.

L (g) before adding fuel to the aeroplane’s fuel tanks, the refuelling equipmentand the aeroplane shall be earthed to the ground and the equipmentconnected to the aeroplane by the use of static lines. The nozzle staticline must be attached to the aeroplane prior to the removal of any fueltank cap;

(h) the fuel is to be filtered into the aeroplane through approved microfilters.If the microfilter is equipped with a drain, the filter shall be drained beforeuse. The person conducting the refuelling shall ensure that the filter(s)have not exceeded their replacement date. ....





(2) Drumstock Refuelling

Oil Company literature warns that drum stock aviation fuels are verysusceptible to contamination from rust, scale and water. Therefore, whenrefuelling from drum stocks the pilot in command must ensure that:

(a) drums have been stored on their side, above the surrounding groundlevel, with the bungs horizontal and, preferably, undercover. This is toprevent water accumulating on the drum head and being drawn into thedrum when cooling takes place during the night. The drums shall be ingood condition, not leaking, original seals are intact and product detailssuch as brand, filling date, grade required (AVGAS; AVTUR (Jet A1)),batch number, etc. are clearly visible and the stock date of the drum hasnot expired. If otherwise, the drum must be rejected;

L (b) each drum should be stood on its end and chocked so that the largebung is on the high side. This will allow sediments or water to settle tothe lowest point of the drum, away from the pump stand pipe;

(c) drums should be left standing for as long as possible and at least for aminimum of 30 minutes, prior for testing for water. In turbine fuel, waterwhen finely dispersed is not visible and takes some time for the water tosettle from suspension;

(d) the drum is then carefully checked for the presence of water. Themethod of water detection is to draw a sample from the lowest point inthe drum by means of a sample tube. This is a small diameter tubesealed at the top by the operator's thumb, inserted to the lowest point ofthe drum and thumb released. This will allow a sample of fuel from thebottom of the drum to be forced into the tube. The operator's thumb isthen replaced over the top of the tube, the tube withdrawn and thesample of fuel placed in a clear clean glass container.

(e) the fuel is checked for colour, clarity and freedom from dirt and/or wateras detailed in 6.3(1)(f) above;

(f) before adding fuel to the aeroplane's fuel tanks, the drum shall beearthed to both the ground and the aeroplane by the use of static lines.The nozzle earth line must be attached to the aeroplane prior to theremoval of the aeroplane's tank cap. The pump, filter and lines shouldbe flushed with a litre or more of fuel;

(g) the fuel is to be filtered into the aeroplane as detailed in 6.3(1)(h); ....





(3) After Fuelling

The pilot in command is responsible for ensuring that:

(a) the aircraft has been refuelled with the correct grade or specification offuel and oil;

(b) the required amount has been dispensed into the aircraft tanks;

(c) sufficient airspace remains in each tank to allow for anticipated expansion;

(d) all fuel and oil tank caps have been securely refitted;

(e) a fuel drain check of each of the aircraft's tanks is carried out with waterdetecting paste or other approved method.

L (f) Where the refuelling, other than hot refuelling, is conducted in theabsence of the pilot in command, the person conducting the refuellingshall inform the pilot of the amount of fuel added and that the refuellinghas been conducted in accordance with this sub-section.

6.4 LOW FLYING OPERATIONS

L (1) Instructions for specialised low flying operations which the Club may conductunder the terms of its Air Operator’s Certificate are contained in Part D. Theapplicable Low Flying Permits are contained in the appropriate CAO or in theCASA Permissions recorded at sub-section 1.2 of Section A1.

(2) The pilot in command of an aircraft engaging in aerial work operations involvingflight below 500 feet AGL is responsible for ensuring that he/she has the requiredlow flying qualification and endorsements where applicable and that all relevantoperational conditions can be complied with. Refer also to the appropriate sectionin Part D relevant to the proposed operation.

(3) When conducting low flying operations, the pilot shall operate below 500 feet onlywhen absolutely necessary and while doing so, shall fly as high as possibleabove the terrain and maintain a continuous lookout for power lines, transmissiontowers, dead trees and other obstacles.

(4) Only persons essential to the operation shall be carried while a Club aeroplaneis engaged in low flying operations. Passengers shall not be carried.

(5) Club pilots engaging in low flying operations should appreciate the importanceof fully understanding the performance data contained in the individual aircraftFlight Manual.

(6) Low flying operations will be conducted only by day in VMC in accordance withthe visual flight rules and in continuous sight of the ground or water asapplicable.


© AEROSERVICE 2000


6.5 NIGHT FLYING OPERATIONS

(1) Night VFR flights are permitted for private and non-passenger carryingcommercial operations provided Night VFR operation is authorised by theindividual aircraft Flight Manual and the pilot meets the requirements of (2).

(2) The pilot in command of any Night VFR flight, other than training flights in thetraffic pattern at night under the VFR as permitted under Part 5 of theRegulations, must be the holder of a private or higher category pilot(aeroplane) licence on which a Night VFR rating has been endorsed, and hascompleted as pilot in command, as pilot in command under supervision or indual flying;

(a) within the previous twelve months, at one flight of at least one hourduration while flying an aeroplane at night;

(b) within the previous six months, carried out at least one take-off andlanding while flying an aeroplane at night;

(c) if carrying passengers within the pervious 90 days, completed threetake-offs and landing at night.

(3) The pilot in command shall ensure that all lighting equipment required inaccordance with sub-section 1.5(5) of Section B1, Part B is on board and isserviceable.

6.6 MERCY FLIGHTS

(1) A Club pilot shall attempt to obtain individual approval from the Chief Pilotbefore endeavouring to obtain an operational concession or making a decisionto declare a mercy flight.

(2) Before declaring a mercy flight, a pilot in command shall endeavour to obtainan operational concession to permit the anticipated irregular operation.Requests for such concessions shall be directed to;

(a) during working hours - the Manager of the nearest District Office of theCivil Aviation Safety Authority;

(b) after hours - the nearest Air Traffic Service unit to obtain the necessarycontact name and telephone number of the appropriate FlyingOperations Inspector. If time does not permit the pilot in command tocontact the Flying Operations Inspector, then a request for assistanceto obtain the concession shall be made to the ATS.


© AEROSERVICE 2000


6.6 MERCY FLIGHTS

(3) If an operational concession cannot be obtained for an urgent medical, flood

or fire relief or evacuation flight in order to relieve a person from grave and

imminent danger and failure to do so is likely to result in loss of life or serious

and permanent disability and the flight will involve irregular operation, it shall

be declared a mercy flight.

(4) The pilot in command is solely responsible for assessing and justifying the

risks involved and for the final decision on whether or not a mercy flight shall

be declared. The factors and risks that the pilot in command must consider

in the declaration, commencement and continuation of a mercy flight are set

out in AIP - MERCY FLIGHTS.

6.7 INSTRUMENT APPROACH RECENCY

(1) The holder of a command instrument rating shall not carry out an instrument

approach using an NDB or VOR in IMC as pilot in command of an aircraft

unless, within the preceding 90 days, that person has performed in flight, or

in a synthetic flight trainer approved for the purpose, an approach using the

same type of navigation aid. An ILS or LLZ approach within the preceding 90

days will satisfy the recency requirements for VOR.

(2) The holder of a command instrument rating shall not carry out an ILS or LLZ

approach in IMC as a pilot in command of an aircraft unless, within the

preceding 35 days, that person has performed in flight, or in a synthetic flight

trainer approved for the purpose, either one of those approaches.

(3) The holder of a command instrument rating shall not carry out an instrument

approach in IMC as pilot in command of an aircraft unless, during the

preceding 15 months, proficiency on the navigation aid being used has been

demonstrated to a flying operations inspector or approved person during an

instrument rating test.

6.8 INSTRUMENT FLIGHT CONTINUATION FLYING

Club pilots shall utilise the Club’s synthetic trainer for continuation instrument flying

training.

....


© AEROSERVICE 2000


6.9 FORMATION FLIGHT

(1) Club aircraft may only engage in formation flight subject to the following

conditions:

(a) The pilots in command shall possess a log book endorsement by a rated

flight instructor certifying competence in aeroplane formation flying.

(b) A formation leader is to be nominated and identified and the names of

all participating pilots shall be clearly recorded or as long as one of the

pilots is an Instructor certified as competent to teach formation flying, the

other pilot does not have to be so endorsed.

(c) Before commencing a formation flight, the leader shall ensure that;

(i) all participating pilots have been briefed on the proposed

manoeuvres and relevant emergency procedures;

(ii) radio communications and visual communications and signals have

been reviewed;

(iii) Air Traffic Control has been notified;

(iv) the flight complies with the requirements of this operations manual.

(2) Training of Club pilots in formation flight shall be in accordance with

sub-section 3.15 of Section E3, Part E.

6.10 TYPE ENDORSEMENT TRAINING

Refer to sub-section 2.5 of Section A2, this Part.





6.11 AEROBATICS

(1) Aerobatic manoeuvres shall only be conducted in Club aircraft which areapproved for aerobatic flight.

(2) A pilot shall not act as pilot in command of a Club aeroplane engaged inaerobatic flight unless his/her pilot's log book has been endorsed permittingthat pilot to execute that particular manoeuvre.

(3) Aerobatic flight shall only be conducted within the boundaries of an approvedaerobatic area unless specific approval has been granted for aerobatic flightat a particular place and time.

(4) The syllabus of training for aerobatic endorsement is contained in sub-section3.14 of Section E3, Part E.

6.12 ACCIDENT AND INCIDENT REPORTING

L (1) The Regulations governing the reporting and investigation of aircraft accidentsand serious incidents (Immediately Reportable Matters) and incidents (RoutineReportable Matters) are contained in Transport Safety InvestigationRegulations 2003 as amended. The AIP - AIR TRAFFIC INCIDENTS containsthe definitions of Immediately Reportable Matters (IRM) and RoutineReportable Matters (RRM) and the contents of the required written report.

L (2) Immediately Reportable Matters

(a) In the event of an accident involving a Club operated aircraft, the pilotin command, the Chief Pilot and the Club management shall be jointlyresponsible for ensuring that a notification of an immediately reportablematter is furnished to the Australian Transport Safety Bureau (ATSB) assoon as reasonably practicable after the occurrence. ATSB phonenumber is 1800 011 034. This is to be followed by a written AIR SAFETY

ACCIDENT OR INCIDENT REPORT within 72 hours;

(b) In addition to complying with the above regulatory requirements, the pilotin command of the aircraft must address a detailed written report to theChief Pilot setting out all the circumstances surrounding that occurrence.

L (3) Routine Reportable Matters

The pilot in command shall furnish a written AIR SAFETY ACCIDENT OR INCIDENT

REPORT to the ATSB within 72 hours following the occurrence.....




6.12 ACCIDENT AND INCIDENT REPORTING

L (4) Completed forms are to be distributed as follows;

(a) Original to ATSB;(b) Copy to the Chief Pilot;(c) Copy to be retained by pilot

L (5) The report must be discussed with the Chief Pilot prior to lodgement so thatadvice may be given on clarification of points, etc. This is not to be taken asan indication that the Club will withhold information or adversely influence thecontext of the report.

L (6) Aviation Self Reporting Scheme

The Club recommends that flight crew make maximum use of the Aviation SelfReporting Scheme (ASRS) to furnish any information, experiences oroccurrences to the ATSB which may relate to air safety. It is stressed that theASRS program is separate from and does not replace the Air Safety Accidentor Incident Reporting system.

L (7) Copies of the AIR SAFETY ACCIDENT OR INCIDENT REPORT and the AVIATION SELF

REPORTING SCHEME REPORT are available from the ATSB by the followingmethods;

(a) by post;

(b) downloaded from the ATSB web site (www.atsb.gov.au); or

(c) completed on line at the ATSB web site

L (8) Statement by Crew Members

(a) All personnel are expected to use due diligence and do and concur indoing, everything reasonably practicable to avoid or diminish any lossinvolving an aircraft owned or operated by this organisation but underno circumstances shall there be any admission of liability or paymentor offer or promise of payment made to any person in respect of anyincident or mishap whatsoever.

(b) No comment shall be made to, or discussion entered into with, anyrepresentative of the press or radio or television or a member of thepublic, without specific authority from management.

L (9) In addition to the regulatory requirements of this sub-section, Club personnelshall follow the procedures shown in Appendix 2 to this Section in the eventof an accident or incident involving a Club aeroplane.


© AEROSERVICE 2000


6.14 SIMULATED ASYMMETRIC FLIGHT

(1) An engine failure should be simulated by slowly closing the throttle. Theapplicable aircraft manufacturer's handbook must be consulted beforeinitiating any simulated engine failure procedure. Simulation of engine failureshall only be conducted by a FOI, ATO or a pilot who is approved to conductmulti-engine training in the aeroplane type.

(2) Simulated engine failure after take-off shall only be initiated by day in VMC.

(3) Practice engine failure after take-off must not be initiated before:

(a) the declared decision point\VSSE has been reached; and

(b) the undercarriage has been retracted (where applicable).

(4) Practice feathering is limited to VMC flights by day during:

(a) type endorsement training;

(b) approved pilot training; and

(c) approved pilot flight tests.

Flight with a feathered propeller on these occasions should be conductedabove 2000 feet AGL except during approach and landing under thesupervision of a person with multi-engine endorsing approval.

(5) Following any practice engine shut-down in flight, the controls must be set foran immediate restart.

(6) Stalling and VMCA demonstrations must not be made with a propellerfeathered or fuel shut off.

(7) Stalling and VMCA demonstrations must not be made when VMCA is less than5 kts above the stall speed for the particular configuration.

(8) Engine out flight is best simulated by setting zero thrust to simulate afeathered propeller.

(9) Consult ATC before conducting asymmetric procedures at any controlledairport and comply with any directions or conditions imposed in respect of thepractice.


© AEROSERVICE 2000


6.15 HAND-OVER AND TAKE-OVER PROCEDURES

(10) In a dual control aircraft, where there are two pilots, it is imperative that therebe no doubt who has physical control of the aircraft at any given time.Accordingly, the following procedure shall be adopted:

(a) When the pilot in command wishes to hand over control he/she will say"handing over" but retain control; the other pilot will then place handsand feet on the controls and say "taking over" at which point the pilot incommand will relinquish control.

(b) When the pilot on command has relinquished control, he/she will say."you have control."

(c) When the pilot in command wishes to again take control, he/she willplace hands and feet on the controls and say "taking over". The otherpilot will remove hands and feet from the controls and say "handing over"and when he/she has handed over, shall add "you have control."

6.16 SIMULATION OF INSTRUMENT FLIGHT

(1) A Club aeroplane shall not be flown under simulated instrument conditionsunless there is a safety pilot on board who has the full amount of forward and sidevision afforded by the particular aeroplane design. This means that screens madeof opaque material must not be used to simulate instrument conditions wherethose screens restrict the vision of the safety pilot.

(2) Pilots should use a tennis shade, an IF visor, two stage amber screens,louvred blinds, or IF glasses acceptable to the CASA.

(3) Practice partial panel (limited panel) flying shall not be instituted at night.

(4) No control instrument shall be failed, obscured or otherwise be madeunavailable to any flight crew member at night.

(5) Any simulated instrument flight shall only be done in VMC and incircumstances where there is no risk to other traffic as a result of thatsimulated flight.

(6) Both pilots on board shall hold an type or class endorsement for the aeroplaneand shall hold a command instrument rating appropriate to the aeroplane typeand the aeroplane in use shall be fitted with fully functioning dual controls andfitted with the flight instruments required for flight under the IFR as specifiedin sub-section 1.5(1)(b), Section B1 of Part B or the safety pilot is a ClubInstructor.

....




6.17 PILOT BRIEFING AND FLIGHT PLANNING INSTRUCTIONS

(1) Pilot Briefing

(a) The pilot in command shall obtain and study information relating to theaerodromes/ALAs, navigation facilities, ATS rules and proceduresNOTAMs and any Club procedures applicable to the route or area ofoperation;.

(b) Information on ALAs is contained in the ALA Register located atAppendix 5 to Section A1, this Part.

(c) Club pilots shall not use any actual or forecast weather reports ofmeteorological conditions unless those reports were made with theauthority of the Director of Meteorology or by a source approved by theCASA. The sources the Club pilots may use are AVFAX, NAIPS,Airservices Internet site or the pilot briefing/Met offices.

L (d) It shall be standard practice to access the AVFAX system or theAirservices Internet site to obtain weather and NOTAM information. Therequired telephone and fax numbers and access codes are shown atAppendix 3 to Section A1, this Part. If fax facilities are not available,pilots may use briefing/Met offices.

(e) All pilots employed by the Club are to thoroughly familiarise themselveswith:

(i) the procedures for access;

(ii) the extent and limits of resources and information available;

(iii) the interpretation of all data available.

(2) Flight Planning

(a) All flight planning associated with the Club's operations shall be carriedout in accordance with the relevant provisions of the AIP/JeppesenAirways Manual and this Operations Manual.

(b) Club pilots shall not conduct a flight under the Visual Flight Rules unlessVisual Meteorological Conditions are forecast to exist over the intendedroute and at the destination for the planned period of the flight. If VMCis not forecast to exist for the proposed flight, Club pilots shall plan theflight as a flight under the Instrument Flight Rules provided the pilot israted and the aircraft has the appropriate equipment for operating underthe IFR;

....





(2) Flight Planning (Cont’d)

L (c) For other than the Clubs regular advertised scenic flight routes and otherlocal flights in the vicinity of YRED, a written flight plan shall be madeusing a standard Airservices Australia Flight Planning Form. This formwill also serve as the Navigation Log.

(3) Fuel Policy

(a) The minimum acceptable fuel for any flight shall be the required flightfuel calculated using the fuel consumption rates, as shown in Appendix1 to Section B2 of Part B, appropriate to the aeroplane type in use, plusany additional fuel as required by (4)(a) and (4)(b) below.

(b) A pilot in command may calculate fuel for a flight on the basis of landingat an intermediate aerodrome, but may continue the flight to thedestination aerodrome if that pilot determines that the remaining fuel onboard, when at or abeam of the intermediate aerodrome, is equal to orgreater than the fuel required in (4)(b) below.

(4) Flight and Reserve Fuel

(a) When calculating the amount of fuel that may be required for a particularflight, allowance should always be made for additional fuel requirementsto cater for:

(i) any holding requirements due to forecast weather conditions en-route or INTER/TEMPO conditions are forecast to exist at thedestination or alternate within the appropriate times before or afterplaned ETA;

(ii) planned air traffic control routing (including departure and arrivalprocedures);

(iii) any delays resulting from traffic holding notified for

- an alternate aerodrome (where required)

- the destination aerodrome;

(b) contingencies such as an engine failure in a multi-engine aeroplane.....


© AEROSERVICE 2000



(4) Flight and Reserve Fuel (Cont'd)

(c) The amount of fuel on board the aircraft at any particular point in a flight

should be an amount that is sufficient to enable the aircraft to fly from

that point:

(i) where an alternate is not required - to 1500 feet above the

destination aerodrome, make an approach and land; or

an alternate is required - make a missed approach to the

destination aerodrome, fly to the alternate aerodrome and make an

approach and land at that aerodrome; plus

(ii) a variable reserve of 15% calculated on the time it would take to fly

in accordance with (c)(I) above; and

(iii) to provide holding fuel as required in (4)(a) above; and

(iv) to provide a fixed fuel reserve of 45 minutes calculated at the

holding rate for the aeroplane at an altitude of 1500 feet above the

destination aerodrome.

NOTE: The variable fuel reserve referred to in (c)(ii) above is nil for

an aeroplane engaged in private or aerial work operations.



© AEROSERVICE 2000


6.18 MINIMUM PILOT EQUIPMENT AND DOCUMENTATION TO BE CARRIED IN FLIGHT

(1) When actually engaged in operations which involve a number of consecutive

flights on the same day from the same place, the minimum pilot equipment

shall be as follows;

- The Aircraft Flight Manual

- The Aircraft manufacturer's handbook (or abbreviated version)

- Flight crew licences and a Valid Medical Certificate

- Current Maintenance Release

- The necessary charts/maps and navigation equipment pertinent to the area

(2) In addition to the equipment carried in (1) above, on all charter and

navigational training flights the minimum pilot equipment shall include

- AIP or Jeppesen Airways Manual

- Current information on ALAs to be used

- Weather forecasts/NOTAMs as applicable

- Passenger Manifest and Flight Record

(3) On all other operations, in addition to the (1) and (2) above, the minimum pilot

equipment shall include

- The Club's Operations Manual

- Flight Authorisation Sheet when conducting training operations



© AEROSERVICE 2000


6.19 PROCEDURES FOR STRAIGHT IN APPROACHES

(1) Pilots operating Club aeroplanes may conduct straight-in approaches at an

uncontrolled aerodrome in a MBZ provided the following provisions are

complied with.

(a) The aircraft must have a serviceable VHF radio to enable

communications on the MBZ frequency associated with the aerodrome

at which the straight-in approach is intended.

(b) All the aircraft's landing lights are serviceable and shall be illuminated

when within 5NM of the aerodrome. Anti-collision lights, including

strobes (where fitted) must also be displayed.

(c) The pilot in command shall determine, by means of radio

communications or visually, the following;

(d) the wind direction

(i) circuit direction

(ii) runway in use

This information may be obtained from ATIS, AWS, UNICOM, other

aircraft operating at the particular aerodrome or visually.

(e) The pilot in command shall determined from NOTAMs, or if NOTAMs are

not issued for the particular aerodrome, from the aerodrome operator,

that the runway to be used is serviceable, and that the aerodrome will be

cleared of ground maintenance equipment and other runway works for

the intended operation. The pilot shall determine if any displaced

threshold is in operation on the runway.

(f) If there is other traffic in the circuit, the pilot in command must use the

runway being used by that traffic unless it is not the into-wind runway, in

which case the into-wind runway may be used.

(g) The aircraft crew shall make the following radio broadcasts;

(i) an "inbound" broadcast outside the MBZ boundary on the MBZ.

- state the intention to carry out a straight-in approach; and

- the runway to be used.

....




6.19 PROCEDURES FOR STRAIGHT IN APPROACHES

(1) Pilots ... may conduct straight-in approaches .... provided the following

provisions are complied with.

(g) The aircraft crew shall make the following radio broadcasts; (Cont'd)

(ii) when established on final approach at 5NM from the aerodrome

state;

- that the aircraft is established on a straight-in approach;

- the runway to be used; and

- the distance from the runway threshold.

NOTE: Club pilots should ensure that the distance is accurately

stated to give the greatest possible assistance to other

aircraft in arranging separation.

(h) Club pilots shall conduct all manoeuvring to establish the aircraft on final

approach outside a 5NM radius from the aerodrome. The pilot shall

establish the aircraft on final approach and aligned with the runway of

intended landing no later than 5NM from the aerodrome.

(i) Club aircraft carrying out a straight-in approach shall give way to any

aircraft flying in the standard circuit pattern if that aircraft is established

on base leg or final approach and is in a position closer to the

aerodrome.

(2) If a Club pilot who is unfamiliar with a particular aerodrome or the straight-in

approach procedures, or who have any doubt about the adequacy of the

aerodrome information available to him/her, that pilot shall join the traffic

pattern in the normal manner and use their own visual observations to ensure

the safety of their operations.



© AEROSERVICE 2000


6.21 USE OF CHECK LISTS

(1) The check lists, as required by CAR 232, which set out the procedures to befollowed during the pre-flight inspections, before and on take-off, in flight,before landing and in abnormal or emergency situations, are contained in theapplicable aircraft Flight Manual, Pilot Operating Handbook or as approved byCASA. Copies of the flight check systems approved by CASA containing thechecklists for Club's operated aeroplanes are shown as Appendixes to thisSection.

(2) Laminated copies of the check lists, referred to in (1) above, for aeroplanesoperated by the Club, are located in each aeroplane and readily available tothe pilot in command, who shall ensure that the check lists are carried out indetail.

NOTE: Transmission of a radio distress message is to form part of all in-flightemergency checklists.

(3) The procedures contained in the normal checklists shall be carried out frommemory, after which the checklist is to be used to confirm all checklist itemshave been actioned. Exterior and interior pre-flight checklists may becompleted from memory without reference to the checklist.

(4) Club pilots shall not carryout checklist procedures while taxying on or crossingan active runway.

6.22 VISUAL AND INSTRUMENT DEPARTURES AND APPROACH PROCEDURES

(1) Departure Procedures

(a) Flight crew are to ensure that their aircraft has been inspected and isready for start up at least 15 mins prior to the scheduled departure time.A start clearance will be requested when required by the ATIS.

(b) All airways clearances are to be noted in writing and clearancealtitudes/flight levels are to be entered on the assigned altitude indicatoron receipt and cleared altitudes/flight levels read back from the assignedaltitude indicator.

(2) Arrival Procedures

(a) Landing Reference Speeds

Club aircraft should arrive at the decision height with approach flapextended and speed not below VY. If a decision to land has been made,landing flap is then to be extended and the aircraft slowed to VREF

depending on the pilot's assessment of environmental factors i.e. steadywind and or gust factor, likely to affect the landing.




6.23 OPERATIONS IN ENVIRONMENTAL EXTREMES

(1) Any instructions or limitations contained in the individual aircraft Flight Manual

and manufacturer's handbook for operating in adverse weather conditions

must be strictly observed.

(2) Considerations for operating in high temperature conditions should include

- minimal use of brakes to avoid overheating;

- releasing the brakes after shutdown to avoid damage due to heat

expansion;

- degradation of take-off performance;

- affect on range performance due to reduction in fuel density;

- draining of fuel tank sumps more often, e.g. before as well as after each

refuelling;

- ensuring that all fuel vents, breather pipes and drain holes remain

completely unobstructed;

- whenever the aircraft is on the ground under surveillance of the pilot and

conditions allow, leave windows and doors open to ventilate the interior.

(3) Aircraft operating in damp humid conditions should be frequently inspected for

evidence of corrosion or lack of lubrication. More frequent inspections should

be made when operating for extended periods in areas of high airborne salt

concentrations and/or high humidity.

NOTE: Use of protective coatings and sealants will help to prevent corrosive

agents from affecting metallic surfaces.

(4) When operating in dusty conditions, more frequent attention should be paid

to the checking and cleaning of engine air inlets and filters to help preserve

engine life.

(5) The maximum demonstrated crosswind component for take-off and landing is

stated in the individual aircraft Flight Manual and that limitation should be

strictly observed.



08/07 FLIGHT CONDUCT A6-22a

L 6.24 USE OF OXYGEN

(1) Where a portable oxygen system is carried, the oxygen system description

and operating instructions are contained in the applicable oxygen system

Manufacturer's Handbook. A copy of the handbook shall be carried on board

the aeroplane when a portable system is to be used.

WARNING

Oil, grease, or other lubricants, soap and other fatty materials constitute

a serious fire hazard when in contact with oxygen. Be sure hands and

clothing are oil-free before handling oxygen equipment. Do not permit

smoking when using oxygen.

(2) The pilot in command shall ensure that the oxygen system is maintained at full

when suitable facilities are available to top the system up.

(3) The pilot in command shall be responsible for ensuring that sufficient oxygen

is available for use, taking into account the number of passengers, planned

flight level and duration, and that all passengers are thoroughly briefed on the

location, operation and donning procedure of the oxygen equipment installed

in the particular aircraft.

(4) Prior to take-off, each crew member shall personally check that his/her oxygen

mask is connected and the system is functioning correctly.

(5) An oxygen mask shall be worn and oxygen used by a crew member whenever

a cabin altitude of 10,000 feet is exceeded.

(6) The pilot in command shall ensure that supplementary oxygen masks are

worn by and oxygen is supplied to all passengers while the cabin altitude is

above 14,000 feet.

(7) The servicing of oxygen systems is to be carried out only by an appropriately

rated LAME.

(8) The precautions to be followed when servicing an oxygen system are detailed

in Appendix 2 to this Section.



08/07 FLIGHT CONDUCT A6-22b



© AEROSERVICE 2000


6.25 DESCENT RATES WITH PASSENGERS ON BOARD

To ensure reasonable passenger comfort, a descent rate of 500 feet per minute

should not be exceeded unless otherwise dictated by an adverse flight condition,

equipment malfunction or ATC requirements.

6.26 TURBULENCE PENETRATION

(1) Thunderstorms, line squalls and other conditions denoting areas of violent

turbulence and/or hail must be regarded as extremely dangerous and be

positively avoided. Avoid flying within 10 kilometres horizontally of a fully

developed cumulonimbus cloud and also directly below the base of the cloud

whenever possible. Vertical air movement capable of producing extremely

severe turbulence is often present near the edge of the cloud's base, or in

clear air below the overhang of the top. An early decision to divert around a

thunderstorm will need a relatively small heading change and result in

minimum distance added to the flight.

(2) When unexpected turbulence is encountered and cannot readily be avoided:

(a) Fasten seat belts and check that all hand baggage and loose items are

securely stowed.

(b) Adjust engine power to the setting that will give the turbulence

penetration or design manoeuvring speed for the aircraft type.

(c) The 'altitude lock' of the auto pilot must be disengaged and if applicable,

'turbulence' mode selected. Whether flying the aircraft manually, or with

the auto pilot, the technique is to maintain attitude control with the

attitude indicator, accepting altitude changes and speed variations whilst

keeping the attitude within safe limits. Roll must be closely controlled,

if a large angle of bank is allowed to develop recovery can be delayed

by turbulence.

(d) Select and maintain a heading that will take the aircraft through the

turbulent area in the shortest time.

(e) Ensure that adequate terrain clearance is maintained by flying at least

the route LSALT plus 1000 feet, more in mountainous areas.

(f) Turn up the cockpit lighting when flying near thunderstorms to minimise

the effect of lightning.


© AEROSERVICE 2000


6.27 FLIGHT IN ICING CONDITIONS

(1) Club aircraft, not approved for flight in icing conditions, shall not be flown in

known or forecast icing conditions.

(2) If a Club aircraft referred to in (1) above inadvertently encounters icing

conditions, the best course of action is to immediately turn back to escape

these conditions and if possible, change the route or altitude to where

conditions are less conducive to icing. Close attention should be given to the

pitot-static system, propellers, induction systems and other components

susceptible to icing.

6.28 NAVIGATION OF CLUB AIRCRAFT

(1) Club aeroplanes shall be navigated in accordance with the following;

(a) Operations under the Instrument Meteorological Conditions;

(i) Club pilots shall use;

- VOR, NDB for tracking and DME/GPS for distance measurement

in the terminal area of an aerodrome; or

- the navigation aid appropriate to the route being flown outside

the terminal area;

in accordance with the navigation requirements, position fixing and

track keeping tolerances specified in the AIP for flight under the

IFR;

(ii) at a cruising altitude/level in accordance with the table of cruising

levels in the AIP for IFR flight unless it is operationally necessary to

cruise at a non-standard level in accordance with an airways

clearance issued by ATC;

(iii) at a height not below the LSALT for the route being flown except

when on a DME/GPS arrival, when under radar control or by day in

V.M.C

(iv) in accordance with an approved instrument approach procedure for

which the pilot has an endorsement in his/her logbook or in

accordance with a visual approach procedure.




6.28 NAVIGATION OF CLUB AIRCRAFT

(1) Club aeroplanes shall be navigated in accordance with the following;

(Cont’d)

(b) Operations under the Visual Meteorological Conditions;

(i) Club pilots shall navigate by the use of World Aeronautical Charts

in accordance with the navigation requirements, position fixing and

track keeping tolerances specified in the AIP for flight under the

VFR;

(ii) NDB, VOR, DME and GPS may be used by Club pilots for position

fixing as an aid to visual navigation;

(iii) pilots shall cruise at a altitude/level in accordance with the table of

cruising levels in the AIP for VFR flight, unless it is operationally

necessary to cruise at a non-standard level in accordance with an

airways clearance issued by ATC.

(iv) at night in VMC, pilots shall not fly below 1000 feet above the

highest obstacle located within 10 miles of the aeroplane except

during takeoff or landing.

(2) Except when arriving or departing from an aerodrome/ALA, while enroute in

the ordinary course of navigation or approved by the CASA and then only in

accordance with any conditions of that approval, the pilot shall remain clear

of any regatta, race meeting or other public gathering,.

L (3) To enable the geographical position of the aeroplane to be determined at any

time the aeroplane is in flight, Club pilots shall utilise the standard Airservices

Australia Flight Planning Form.

6.29 MARSHALLING AND PARKING OF AIRCRAFT

(1) Where the Club provides ground marshalling, the signals used shall be as

detailed in CAO 20.3 Appendix I.

(2) Club aeroplanes shall be parked in designated parking bays or areas or, if

parking areas are not designated, in an area where the aeroplane will not

cause inconvenience to other aerodrome users.




6.30 OVERWATER OPERATIONS

(1) Club pilots shall not plan a flight over water in a Club operated single-engineaeroplane below a height that would allow the aeroplane to reach land in theevent of engine failure except when the following conditions are met;

(a) each person on board has ready access to a life jacket and wears a lifejacket when the aircraft is operating below 2000 feet AGL;

(b) a meteorological forecast is obtained;

(c) the flight operates on a reporting schedule with Airservices when actuallyoperating overwater; and

(d) if conducting a passenger carrying charter operation, the distancebetween successive land areas suitable for an emergency landing doesnot exceed 50 nm.

(2) Club operated multi-engine aeroplanes conducting overwater operations shallnot plan or operate over water unless;

(a) the aeroplane is not operated over a route in metrological conditions orat a weight that would preclude the aeroplane reaching a suitableaerodrome in the event of the failure of the critical engine;

(b) the aeroplane is equipped and navigated in accordance with thenavigation requirements and track keeping tolerances specified in theAIP for flight under the IFR; and

L (c) if operating at a distance greater than 50 nm from land or when the take-off or approach path is so disposed over water that, in the event of amishap occurring during these phases of flight, the aircraft would beforced into the water, a life jacket shall be provided for each person onboard; and

(d) if operating outside a distance equal to 30 minutes at the normal cruisingspeed of the aeroplane in use, or 100 miles, whichever is the less, a liferaft of sufficient capacity to accommodate all the persons on board shallbe carried.

L (3) The above conditions for the wearing of life jackets do not apply whenconducting aerial work operations and the aircraft is departing from, or landingat a landing site in the normal course of navigation for departing from orlanding at that landing site.

L (4) Where a life raft is carried, the following additional items shall be carried;

(a) a survival kit suitable for a marine environment;

(b) a survival radio beacon meeting the requirements of CAR 252A(5) and

(c) a supply of pyrotechnic distress flares.


© AEROSERVICE 2000


6.31 AIREPS

(1) The pilot in command of a Club aeroplane shall report at times requested by

a metrological observer the meteorological conditions observed enroute.

Position reporting points which require the addition of meteorological

conditions observed are shown in AIP MAP.

(2) If the pilot in command of a Club aeroplane observes meteorological

conditions enroute which are of a hazardous to flight or are substantially

different to that forecast, the pilot shall report those meteorological conditions

to the appropriate authority.

6.32 DETERMINATION OF VISIBILITY AND CLOUD BASE

(1) The pilot in command must, prior to each take off, ensure that the required

visibility and cloud base exists to permit the intended operation. All available

approved sources of information should be used such as ATIS, Tower

observations, Automatic Weather Information Broadcast (AWIB), Automatic

En Route Information Service (AERIS), METAR, SPECI, TTF, TAF, SIGMET,

AIRMET, Flight Watch facilities and by personal observation.

(2) In flight, the pilot in command will determine whether the existing conditions

are suitable to continue the current flight or approach and landing or whether

alternative action such as a missed approach, holding, diversion, delay or

cancellation of the flight is necessary.

6.33 AIRCRAFT WEIGHT AND PERFORMANCE LIMITATIONS

(1) The pilot in command of a Club aeroplane is responsible for determining that

the aircraft can meet the requirements of CAO 20.7.4.

In some cases the required gradients on climb, enroute and approach

procedures exceed the required standard and the pilot in command may need

to consider action to be taken should an engine fail. This may include a

reduction in weight, different flight path, circling over the top of the aerodrome

until LSALT is achieved or in some cases a determination that it is not

possible to operate at a particular aerodrome.

....


© AEROSERVICE 2000



(2) The pilot in command shall only operate a Club aeroplane at the lesser take-

off weight which allows;

(a) a take-off distance that is equal to or less than the distance determined

from the take-off weight chart in the applicable aircraft Flight Manual;

(b) a climb gradient of 6% at take-off safety speed in the take-off

configuration, without ground effect and with all engines operating at

take-off power. Multi-engine aeroplanes below 5700 kg certified in the

normal, utility and acrobatic category (CAO 101.22) meet this requirement.

(c) an en-route climb gradient of 1% at all heights up to 5000 feet in ISA in

multi-engine aeroplanes operating under the IFR on charter operations

in the following configuration;

- propeller of the critical inoperative engine stopped;

- the undercarriage and flaps retracted;

- the remaining engine(s) operating at maximum continuous power.

This weight shall be determined from The Performance Section in the

applicable Pilot's Operating Handbook.

(d) after allowance for fuel used;

(i) a landing distance at the destination and alternate airports which is

equal to or greater than the distance determined from the landing

weight chart in the applicable aircraft Flight Manual; or

(ii) a weight which allows a landing climb performance of 3.2% in ISA with

all engine operating at take-off power at a speed not exceeding 1.3VS.

This weight shall be determined from The Performance Section in

the applicable Pilot's Operating Handbook.

(3) The pilot in command shall only operate a Club aeroplane at a landing weight

which allows a landing distance that is equal to or less than the distance

determined from the landing weight chart in the applicable aircraft Flight

Manual.

....


© AEROSERVICE 2000



(4) The pilot in command of a Club operated aeroplane shall use;

(a) the actual pressure, temperature and wind component or the declared

density altitude charts in CAO 20.7.0 for the purpose of determining

landing weight limitations at the time of landing;

(b) the forecast pressure and temperature or approved declared conditions

and zero wind component for determining the maximum landing weight

at the time of planning.

(5) Club single-engine aeroplanes shall not be operated at night under the Visual

Flight Rules except when engaged in private, aerial work or non-passenger

carrying charter operations.

6.34 OPERATIONAL PROCEDURES IN RELATION TO COMPUTERS

(1) The pilot in command of a Club aeroplane shall ensure that;

(a) the current amendment data is being used in any Nav Data base or;

(b) if any information is loaded manually e.g. a flight plan created, then the

information loaded is to be checked for accuracy before use and at each

turning or way point a reasonableness check is carried out (track and

distance to next way point);

(2) If at any time the computer generated output appears in error, be prepared to

revert to basic visual navigation procedures.GG

© AEROSERVICE 2000

08/00 THE REDCLIFFE AERO CLUB Section A6FLIGHT CONDUCT Appendix 1


NAVIGATION LOG

AIRCRAFT: PILOT: DATE:

PSN/ETD LSALT FL/ALT TAS TRK(M) WIND HDG(M) G/S DIST ETIPLD

EST

REV

EST

ATD

ATA

FROM

MIN L/KG MIN L/KG MIN L/KG MIN L/KG MIN L/KG MIN L/KG

CLIMB

CRUISE

DESCENT

ALTERNATE

FLIGHT FUEL

VARIABLE RES

FIXED RES

TRAFFIC HOLDING

WEATHER HOLDING

TAXI

REQ FUEL

MARGIN FUEL

TOTAL FUEL

BRIEFING 1800 805 150 FAX 1800 805 747 PILOT PC ACCESS 1800 059 999 CENSAR 1800 814 931

SARTIME: DATE TIME: TO ATS UNIT: FOR ARRIVAL AT: LAST LIGHT:

AMD 10


FLIGHT CONDUCT Appendix 2

Page 1

CHECKLISTS FOR CLUB AEROPLANES

Aircraft Page

CESSNA C150/C152 3

CESSNA C172 7

CESSNA C177 11

CESSNA U206G 15

CESSNA 210M 19

PIPER PA28-181 25

PIPER PA28R-200 29

PIPER PA32-300 33

PIPER TWIN COMANCHE PA30-160B 37

GRUMMAN AMERICAN AA-5B 41

SKYFOX GAZELLE CA25N 45

PIPER PA28-151 47

PA-38-112 PIPER TOMAHAWK 50

COMMANDER 112 55

BEECHCRAFT BONANZA 36, A36 63

DE HAVILLAND TIGER MOTH DH-82A 69

CESSNA MODEL 182 73

AMD 14



Page 2

CHECKLISTS FOR CLUB AEROPLANES

Aircraft Page

PARTENAVIA PN68 AEROPLANES 77

SUPER DECATHLON 8KCAB 83

CESSNA 310R 89

CITABRIA 7GCAA 99

CESSNA 172S (SP) 103

PIPER PA31-350 105

LPA-32R-301T, SARATOGA H TC 117

LPA-44-180T, TURBO SEMINOLE 127



Page 3

CESSNA C150/C152

Pre flight information and emergency procedures as per Cessna Model 152 Information

Manual Part No. D1210-13-RPC-200-2/83 and Cessna Model 150 Information Manual Part

No. D1013-13-RGI-200-10/97. Pilots should read the Operator's Handbook prior to flight.

BASIC AEROPLANE OPERATING CHECK LIST

PRE START

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

All Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Radios & Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Beacon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Master . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked

Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On and sufficient

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

Prime . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . If required & locked

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

All Clear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START

POST START

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Normal

Ampere Meter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked

Radio & Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Flaps UP

TAXYING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Working

Gyro Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Working


Page 4CESSNA C150/C152

PRE TAKE OFF

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMFRICTION NUT FIRM

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHPrimer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOCKEDFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & SUFFICIENTFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETTrim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREE & FULL MOVEMENTCircuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDInstruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED INDIVIDUALLY

RUN UP

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET 1700 RPMMag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDOil pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDOil Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDCarby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDIdling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECUREHatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE & LOCKEDSeats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

LINE UP

Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONDG/Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

AFTER TAKE OFF

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL POWEROil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDOil Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED



Page 5

CESSNA C150/C152

PRE LANDING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EQUAL PRESSURE & OFF

Undercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN & LOCKED

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & SUFFICIENT

Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Hatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

BASE LEG

Carby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 DEGREES

FINAL

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

Carby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF


AFTER LANDING (clear of runway)

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDBY

Strobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF



Page 6

CESSNA C150/C152

SHUT DOWN

Radio & Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

Mag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLY LEAN

Mag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Master . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Control Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FITTED

Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STOWED

Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

INTERCIRCUIT

Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & SUFFICIENT

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1700 RPM


Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Hatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE



Page 7

CESSNA C172

Pre flight inspection and emergency procedures as per Cessna Model 172 Information

Manual Part No. D 1138-1 3-RGI-3000


PRE START

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

All Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Radios & Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Beacon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Master . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & SUFFICIENT

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

Prime . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IF REQUIRED & LOCKED

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

All Clear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START

POST START

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMAL

Ampere Meter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Radio & Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

TAXYING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKING

Gyro Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKING



Page 8

CESSNA C172

PRE TAKE-OFF

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FRICTION NUT FIRM

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

Primer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOCKED

Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & SUFFICIENT

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREE & FULL MOVEMENT

Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED INDIVIDUALLY

RUN UP

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET 1700 RPM


Oil pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Oil Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Suction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Carby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Idling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Hatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE & LOCKED

Seats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

LINE UP

Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Strobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

DG/Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED



Page 9

CESSNA C172

AFTER TAKE OFF

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL POWER

Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

Oil Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

PRE LANDING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EQUAL PRESSURE & OFF


Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & SUFFICIENT

Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Hatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

BASE LEG

Carby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 DEGREES

FINAL

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

Carby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF


AFTER LANDING (clear of runway)

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDBY

Strobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF



Page 10

CESSNA C172

SHUT DOWN

Radio & Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM


Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLY LEAN

Mag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Master . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Control Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FITTED

Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STOWED

Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

INTER CIRCUIT

Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & SUFFICIENT

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1700 RPM


Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Hatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE



Page 11CESSNA C177

Pre flight inspections and emergency procedures as per Cessna Model 177 InformationManual.

BASIC AEROPLANE OPERATING CHECKLIST

PRE FLIGHT

Authorisation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETEMaintenance Release . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECTED AND SIGNEDPre-flight inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS PER HANDBOOKBaggage . . . . . . . . . . . . . . . . . . . . . . . . . . . BAGGAGE AREA SECURE AND LOCKEDMandatory Documents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ABOARDTrip Sheet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOG START TIMEStart Position Suitable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SUITABLE

PRE START

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENAll Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFRadio and Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFBeacon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONCircuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON BOTHMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHProp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL FINECarburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COLDPrime . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 STROKESThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET 1/2 INCHMagnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTHAll Clear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START

POST START

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET RPM 1000Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GREENOil Temps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INDICATIONSAmpere Meter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INDICATEDRadio und Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

TAXYINGBrake Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK PRESSUREDG & Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKTum Co-ordinator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK


Page 12CESSNA C177

PRE TAKE-OFF

Park Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONTrims . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETThrottle Friction Nut . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH (BELOW 3000)

(Lean Rich At High Density Altitudes Refer Information Manual)Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON BOTHFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (THEN OFF)Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET 0-10 (10 PREFERRED)Instruments Flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETInstruments Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

RUNUP

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1800 RPMMag Switches Left/Right . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK(RPM Drop Should Not Exceed 150 RPM on Either Magneto or 50 RPM DifferentialBetween Magnetos )Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CYCLE

(CHECK FEATHER 500 RPM MAX)Carburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FOR RPM DROPAmmeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSuction Gyro . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSwitches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKCircuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKHatches and Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

LINE UP

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHDG & Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON ALTStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

AFTER TAKE OFF

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCEFuel Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Temp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK


Page 13CESSNA C177

TOP OF CLIMB

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEANCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSEDArea QNH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

TOP OF DESCENT

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETCarby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDLocal QNH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

PRE LANDING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EQUAL PRESSURE AND OFFUndercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN LOCKEDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON BOTH AND SUFFICIENTOil TS & Ps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKHarness & Hatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

BASE

Carby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 Deg

FINAL

Pitch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP (FULL FINE )Undercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN AND LOCKEDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

AFTER LANDING

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDBYStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFCarby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF


Page 14CESSNA C177

SHUTDOWN

Radios and Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMMags L/R . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUTOFFMags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMaster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFControl Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FITTEDFuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RIGHTHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STOWEDDoors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED


Page 15CESSNA U206G

Pre flight inspections and emergency procedures as per Cessna U206G manufacturer’sManual. 1981 - Revision 1-5 Dec 1980/D1203-1-13PH-RPC450-1/81


BEFORE STARTING ENGINE

Pre flight Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETESeats, Seat Belts, Shoulder Harnesses . . . . . . . . . . . . . . . . . . . . . . . ADJUST & LOCKBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST & SETCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENAvionics Power Switch, Autopilot (if Installed), Electrical Equipment . . . . . . . . . . . OFF

CAUTION

The avionics switch must be off during enginestart to prevent possible damage to avionics.

Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLER TANKCircuit Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IN

STARTING ENGINE

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPMThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSEDAuxiliary Fuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE

to obtain 8-10 gal/hr flow, then return to CLOSED positionAuxiliary Fuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFPropeller Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEARIgnition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STARTThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE slowlyIgnition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE when engine starts

Note

The engine should start in two or three revolutions. If it does not continue running, startagain at step 3 above. If the engine does not start, leave auxiliary fuel pump switch off,set mixture to idle cut-off, open throttle, and crank until engine fires or for approximately15 seconds. If still unsuccessful, start again using the normal starting procedure afterallowing the starter motor to cool.

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLEOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKFlashing Beacon and Navigation Lights . . . . . . . . . . . . . . . . . . . . . . . . . ON as requiredAvionics Power Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON


Page 16CESSNA U206G

BEFORE TAKEOFF

Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETCabin Doors and Window . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED & LOCKEDCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENFlight Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREE & CORRECTFuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLER TANKAuxiliary Fuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH (below 3000 ft)Elevator and Rudder Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TAKEOFF settingThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1700 RPM

a) Magnetos - CHECK (RPM drop should not exceed 150 RPM on either magnetoor 50 RPM differential between magnetos)

b) Propeller - CYCLE from high to low RPM; return to high RPM (full forward)c) Engine Instruments and Ammeter - CHECKd) Suction gauge - CHECK

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETAutopilot (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFStrobe Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIREDThrottle Friction Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUSTParking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE

TAKEOFF

NORMAL TAKEOFFWing flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0°-20°Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE & 2850 RPMMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN for field elevation per fuel flow placardElevator Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LIFT NOSE WHEEL at 50 KIASClimb Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70-80 KIASWing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT after obstacles are cleared

SHORT FIELD TAKEOFFWing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20°Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLYPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE and 2850 RPMMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN for field elevation per fuel flow placardBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASEElevator Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . SLIGHTLY TAIL-LOW ATTITUDEClimb Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65 KIAS until all obstacles are clearedWing Flaps . . . . . . . . . . RETRACT after obstacles are cleared and 80 KIAS is reached

NOTEDo not reduce power until wing flaps have been retracted


Page 17CESSNA U206G

ENROUTE CLIMB

NORMAL CLIMBAirspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 90-100 KIASPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 INCHES Hg & 2250 RPMMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN

to 18 gal/hr fuel flowCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN as required

MAXIMUM PERFORMANCE CLIMBAirspeed . . . . . . . . . . . . . . . . . . . . . . . . . 84 KIAS at sea level to 78 KIAS at 10,000 feetPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE & 2700 RPMMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN for altitude per fuel flow placardCowl flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

CRUISE

Power . . . . . . . . . . . . . . . . . . 15-25 INCHES Hg, 2200-2550 RPM (no more than 75%)Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN

for cruise fuel flow as determined from your Cessna Power Computer or inaccordance with the cruise data in Section 5 of Pilot's Operating Handbook

Elevator and Rudder Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUSTCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

DESCENTPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIREDAuxiliary Fuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN

for smoothness in power descents. Use full rich mixture for idle powerCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

BEFORE LANDINGFuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLER TANKAuxiliary Fuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH (below 3000 ft)Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPMAutopilot (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

LANDING

NORMAL LANDINGAirspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75-85 KIAS (flaps up)Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

(0°- 10° below 140 KIAS, 10°-40° below 100 KIAS)Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65-75 KIAS (flaps DOWN)Elevator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUSTTouchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRSTLanding Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOWER NOSE WHEEL GENTLYBraking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MINIMUM REQUIRED


Page 18



Page 19CESSNA 210M

Pre flight inspections and emergency procedures as per Cessna 210M manufacturer’sManual.



Pre flight Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETESeats, Seat Belts, Shoulder Harnesses . . . . . . . . . . . . . . . . . . . . . . . ADJUST & LOCKBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST & SETCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

(move lever out of locking hole to reposition)Avionics Power Switch, Autopilot (if Installed), Electrical Equipment . . . . . . . . . . . OFF

CAUTION

The avionics switch must be off during enginestart to prevent possible damage to avionics.

Landing Gear Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWNMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONLanding Gear Lights and Horn . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS TO TESTCircuit Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK INFuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLER TANK

STARTING ENGINE

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPMThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSEDAuxiliary Fuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE

to obtain 50-60 lbs/hr flow, then RETURN to IDLE POSITIONAuxiliary Fuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFPropeller Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEARIgnition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STARTThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE slowlyIgnition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE when engine starts

Note

The engine should start in two or three revolutions. If it does not continue running, startagain at step 3 above. If the engine does not start, leave auxiliary fuel pump switch off,set mixture to idle cut-off, open throttle, and crank until engine fires or for approximately15 seconds. If still unsuccessful, start again using the normal starting procedure afterallowing the starter motor to cool.

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESET to desired IDLE speedOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK


Page 20CESSNA 210M

BEFORE TAKEOFF

Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETCabin Doors and Window . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED & LOCKEDCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPENFlight Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREE & CORRECTFlight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKFuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLER TANKAuxiliary Fuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH (below 3000ft)Elevator and Rudder Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TAKEOFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1700 RPM

a) Magnetos - CHECK (RPM drop should not exceed 150 RPM on either magnetoor 50 RPM differential between magnetos)

b) Propeller - CYCLE from high to low RPM; return to high RPM (full forward)c) Engine Instruments and Ammeter - CHECKd) Suction gauge - CHECK in green arc

Avionics Power Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETAutopilot (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFFlashing Beacon, Navigation Lights and/or Strobe Lights . . . . . . . . ON AS REQUIREDThrottle Friction Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUSTParking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE

TAKEOFF

NORMAL TAKEOFFWing flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0°-10° (10° preferred)Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE & 2850 RPMMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN

for field elevation per fuel flow placard ABOVE 3000 FTElevator Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . LIFT NOSE WHEEL at 60-70 KIAS

NOTE

When the nose wheel is lifted the gear motor mayrun 2-3 seconds to restore hydraulic pressure

Climb Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80-90 KIASBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY momentarily when airborneLanding Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT to climb outWing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT

AMD 1


Page 21CESSNA 210M

SHORT FIELD TAKEOFFWing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20°Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLYPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE and 2850 RPMMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

Lean for field elevation per fuel flow placard ABOVE 3000 FTBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASEElevator Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SLIGHTLY TAIL-LOW ATTITUDEClimb Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . 71 KIAS until all obstacles are clearedLanding Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT after obstacles are clearedWing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT after reaching 80 KIAS

NOTEDo not reduce power until wing flaps and landing gear have been retracted

ENROUTE CLIMB

NORMAL CLIMBAirspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 100-110 KIASPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 INCHES Hg & 2250 RPMMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN to 108 lbs/hrCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN as required

MAXIMUM PERFORMANCE CLIMBAirspeed . . . . . . . . . . . . . . . . . . . . . . . . . 97 KIAS at sea level to 90 KIAS at 10,000 feetPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE & 2700 RPMMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN for altitude per fuel flow placardCowl flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPEN

CRUISE

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15-25 INCHES Hg, 2200-2550 RPM(no more than 75%)

Elevator and Rudder Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUSTMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN

as per your Cessna Power Computeror the cruise data in Section 5 of Pilot's Operating Handbook

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED (open if required)

DESCENT

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIREDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST

for smooth operation (full rich mixture for idle power)Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

AMD 1


Page 22CESSNA 210M

BEFORE LANDING

Seats, Belts, Shoulder Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECUREFuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLER TANKLanding gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EXTEND (below 140 KIAS)Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH (below 3000 ft)Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPMWing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

(0°- 10° below 150 KIAS, 10°-30° below 115 KIAS)Autopilot (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFElevator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST

LANDING

NORMAL LANDINGAirspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80-90 KIAS (flaps up)Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

(Flaps down preferred)Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70-80 KIAS (flaps DOWN)Elevator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUSTTouchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRSTLanding Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOWER NOSE WHEEL GENTLYBraking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MINIMUM REQUIRED

SHORT FIELD LANDINGWing flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL DOWNAirspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 71 KIASElevator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUSTPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE to idle after clearing obstacleTouchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRSTBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY HEAVILY Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT

BALKED LANDINGPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE 2850 RPMWing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT to 20° (immediately)Climb Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 KIAS (until obstacles are cleared)Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

(lean for field elevation per fuel flow placard above 3000 feet)Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT slowly

(after reaching safe altitude and 75-80 KIAS)Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN


Page 23CESSNA 210M

AFTER LANDINGWing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACTCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENRadar (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

SECURING AEROPLANEParking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETAvionics Power Switch, Electrical Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUTOFF (pulled full out)Ignition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFControl Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSTALL


Page 24



Page 25PIPER PA28-181

Pre flight inspections and emergency procedures as per Piper Cherokee Archer IIPA28-181 Manufacturers Information Manual report: VB-790 issued June 18 1976.


PRE FLIGHT

Authorisation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETEMaintenance Release . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECTED AND SIGNEDPre flight inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS PER HANDBOOKBaggage . . . . . . . . . . . . . . . . . . . . . . . . . . . BAGGAGE AREA SECURE AND LOCKEDMandatory Documents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ABOARDTrip Sheet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOG START TIMEStart Position Suitable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SUITABLE

PRE START

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONCarb Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL COLDFuel Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DESIRED TANKThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1/4 INCH OPENMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKIF ENGINE DOES NOT START Within 10 sec PRIME AND REPEAT STARTINGPROCEDURE

STARTING ENGINE WHEN HOT

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1/2 INCH OPENMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set 1000 RPMOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK



FLOODED STARTThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPENMaster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT OFFStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETARDOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

POST START Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

TAXYINGBrake Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKDG & Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKTurn Co-ordinator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSteering . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

PRE TAKE-OFF Park Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2000 RPMMags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX DROP 175 RPM - MAX DIFF 50 RPMVacuum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.0 Hg ±Oil Temp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKAnnunciator Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS TO TESTCarby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFFuel Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IDLEMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFlight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKFuel Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLEST TANKElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONEngine Gauges . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKCarby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFSeat Backs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE & ERECTMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETBelts/ Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENEDEmpty Seats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SEAT BELTS SNUGLY FASTENEDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETTrim Tabs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL & FREE MOVEMENTDoors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LATCHED

Engine is warm for take off when throttle can be opened without engine faltering.



LINE UP Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHFuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONDG & Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ALT ON

AFTER TAKE OFF Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPTrim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF/ CHECK PRESSUREOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Temp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

PRE LANDING Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKUndercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWNMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLEST TANKOil Ts &Ps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKHarness & Hatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

AFTER LANDING

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDBYStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

SHUTDOWN

Electric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMMags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUTOFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL ARFTMags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMaster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECUREHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STOWEDDoors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED


Page 28



Page 29PIPER PA28R-200

Pre flight inspection and emergency procedures as per Piper Arrow PA28R-200 Serial No.28R-7235001 though 28R-7335446.Manufacturers Information Manual Part No.761493.


PRE START

Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONGear Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK GREENFuel Quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK GAUGESTrim Tabs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN 20 mmProp Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FORWARDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

(Indication of fuel flow)Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUTOFFMag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ALL CLEARStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE

POST START

Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKRadios & Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON



TAXYING Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKDG & Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKTurn Co-ordinator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

PRE TAKE-OFF

Park Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONTrims . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETThrottle Friction Nut . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & FULLEST TANKFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETInstruments (Flight) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETInstruments (Engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMMag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK 4.8/5.1Ampere Meter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1700 RPMPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EXERCISE

(Check feather 500 rpm max.) Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IDLEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 PMPitot Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKHatches/Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

LINE UP

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONDG & Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON



AFTER TAKE-OFF

Undercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCEFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFFuel Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

TOP OF CLIMB

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEANEDArea QNH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

TOP OF DESCENT

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETLocal QNH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETTraffic . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESOLVED

PRE LANDING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKUndercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN & LOCKEDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLEST TANKFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFuel Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKHatches/Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK



FINAL

Pitch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP (full fine)Undercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN and LOCKEDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

MISSED APPROACH

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPitch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPGear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFlap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP (in stages)

AFTER LANDING

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDBYStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

SHUT DOWN

Radio & Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMMag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLY LEANMag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMaster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STOWED



Pre flight inspection and emergency procedures as per Piper Cherokee Six 300 PA32-300Serial No. 32-7940073 Manufacturers Information Manual Part No. 753745


PRE START

Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONGear Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK GREENFuel Quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK GAUGESTrim Tabs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN 20mmProp Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FORWARDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON(Indication of fuel flow)Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUTOFFMag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ALL CLEARStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE

POST START

Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKRadios & Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON



TAXYING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKDG and Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKTurn Co-ordinator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

PRE TAKE OFF

Park Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONTrims . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETThrottle Friction Nut . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & FULLEST TANKFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETInstruments (Flight) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETInstruments (Engine) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2000 RPMMag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK 4.8/5.1Ampere Meter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1700 RPMPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EXERCISE(Check feather 500 rpm max.) Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IDLEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMPitot Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKHatches/Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

LINE UP

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONDG & Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON



AFTER TAKE OFF

Undercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCEFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFFuel Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

TOP OF CLIMB

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEANEDArea QNH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

TOP OF DESCENT

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETLocal QNH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETTraffic . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESOLVED

PRE LANDING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKUndercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN & LOCKEDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLEST TANKFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFuel Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKHatches/Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK



FINAL

Pitch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP (full fine)Undercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN and LOCKEDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

MISSED APPROACH

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPitch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPGear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFlap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

(in stages)

AFTER LANDING

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDBYStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

SHUT DOWN

Radio & Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMMag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLY LEANMag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMaster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STOWED


Page 37PIPER TWIN COMANCHE PA30-160B

Pre flight inspections and emergency procedures as per Piper Twin Comanche PA30-160B manufactures manual.


PRE FLIGHT

Authorisation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETEMaintenance R..ease . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECTED AND SIGNEDPre flight inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS PER HANDBOOKBaggage . . . . . . . . . . . . . . . . . . . . . . . . . . . BAGGAGE AREA SECURE AND LOCKEDMandatory Documents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ABOARDTrip Sheet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOG START TIMEStart Position Suitable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SUITABLE

PRE START

Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONGear Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK GREENFuel Quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK GAUGESCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENTrim Tab . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETThrottles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN 20mmProp Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FORWARDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON (INDICATION OF FUEL FLOW)Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUTOFFMags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONPropellers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEARStarters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEMixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE

FLOODED START

Mags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONThrottles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENMixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUTOFFFuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFStarters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGE

(WHEN ENGINE FIRES < RETARD THROTTLE AND ADVANCE MIXTURES)



POST START Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMALSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKAlternators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONAvionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONTaxi Clearance

TAXYING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKING DG & Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKING Tum CO Ordinator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKING

PRE TAKE-OFF

Park Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONTrims . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TAKEOFFThrottle Friction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETMixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON/ LINEUPFuel Mains . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFlaps Set . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TAKE-OFFInstruments Flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETInstruments Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

RUN UP

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2200 rpmMags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.8/5.1 CHECKAlternator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKThrottles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1500 rpmProp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EXERCISE (CHECK FEATHER rpm MAX)Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CHECKThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 rpmSwitches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONLights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDPitot Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKCircuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKHatches & Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECUREAirways Clearance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RECEIVEDSafety Brief . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GIVEN



LINE UP

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHFuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONDG & Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDPitot Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDRadios/ DME . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET LOUD

AFTER TAKE OFF

Undercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCEFuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFFuel Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Ts & Ps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

TOP OF CLIMB

Climb Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSEDArea QNH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEANED

CRUISE

ETA Next Position . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DONEDescent Point . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DONENavaids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDENTIFIEDTraffic . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESOLVEDFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SELECTED

PRE LANDING

Blakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EQUAL PRESSURE & OFFUndercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN AND LOCKEDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAINSFuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONOil TS & Ps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKHarness & Hatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE



FINAL CHECKS

Pitch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPUndercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWNCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

SHUTDOWN

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 rpmRadio and Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKMixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLY LEANMags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMaster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STOWED


Page 41GRUMMAN AMERICAN AA-5B

Pre flight inspections and emergency procedures as per Grumman American Model AA-5B Manufacturers Manual Part No. AA5B-137-RAND-4000-11/74 .


PRE FLIGHT

Authorisation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETEMaintenance Release . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECTED AND SIGNEDPre flight inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS PER HANDBOOKBaggage . . . . . . . . . . . . . . . . . . . . . . . . . . . BAGGAGE AREA SECURE AND LOCKEDMandatory Documents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ABOARDTrip Sheet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOG START TIMEStart Position Suitable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SUITABLE

PRE START

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLEST TANKPrimer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN 1/4 INCHCarb Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMaster/Alt. Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONAux Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON (0.5-8 psi )Aux Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFCLEAR PROPIgnition Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTHStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS

POST START

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 rpmOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMALSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONAmpere . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

TAXYING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKINGDG & Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKINGTurn Coordinator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKING



PRE TAKE-OFF

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK OPERATIONFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPTrim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETPrimer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOCKEDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHCarby Heal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKInstruments Flight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETInstruments Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKCanopy . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKAux Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

RUN UP

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET 1800 rpmEngine Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKMags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (175 rpm EACH MAX DIFF 50 rpm)Carby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

LINE UP

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHFuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONDG & Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

AFTER TAKE OFF

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL POWEROil Ts & Ps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED



CRUISE

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2200 TO 2700 rpmAux Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFLean Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDFuel Quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

PRE LANDING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FULLEST Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TANKAux Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHCarb Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDOil TS & Ps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKHarness & Hatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

AFTER LANDING

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPCarby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAux Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

SHUTDOWN

Electric Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMag S`vitches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLY LEANMags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMaster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STOWED


Page 44



Page 45SKYFOX GAZELLE CA25N

Pre flight inspections and emergency procedures as per Skyfox CA25N Gazelle CivilAviation Safety Authority flight manual revised July 1995.


PRE FLIGHT

Authorisation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETEMaintenance Release . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECTED AND SIGNEDPre flight inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS PER HANDBOOKBaggage . . . . . . . . . . . . . . . . . . . . . . . . . . . BAGGAGE AREA SECURE AND LOCKEDMandator Documents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ABOARDTrip Sheet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOG START TIMEStart Position Suitable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SUITABLE

PRE START Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONAll Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF EXCEPT ALTERNATORRadio and Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMaster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONCircuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON AND VISUALLY CHECK CONTENTSThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET APPROX 3mrnFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON {Clicking]Choke . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON IF COLDCDI Switches, . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONAll Clear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START {starter button]

WARM UP AT 2500 RPM

POST START Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMALVoltmeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GREEN RANGERadio and Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

TAXYINGBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKINGGyro Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKING

PRE TAKE-OFF Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2500 RPM

FRICTION NUT FIRMFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON AND SUFFICIENTFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElevator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREE AND FULL MOVEMENTCircuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED INDIVIDUALLY


Page 46SKYFOX GAZELLE CA25N

RUN UPBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3850 RPMCDI Switched . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED INDIVIDUALLY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP TO 300 RPM DROP IS ACCEPTABLEMAX 115 RPM DIFFERENCECarby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDVoltmeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GREEN RANGEIdling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1600 - 1800 RPMThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2500 RPMHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECUREHatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE AND LOCKEDSeats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

LINE UP Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONDG/Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED

AFTER TAKE OFF Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL POWER

CHECK ENGINE INSTRUMENTS FOR NORMAL INDICATIONS

PRE LANDING Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EQUAL PRESSURE & OFFUndercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN AND LOCKEDFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & SUFFICIENTHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECUREHatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

SHUTDOWN Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2500 RPMRadio and Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFCDl's . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTH OFFMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STOWED

INTERCIRCUIT Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & SUFFICIENTThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3850 RPMCDI Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2500 RPMHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECUREHatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

AMD 7



Pre flight inspections and emergency procedures as per Piper Cherokee Warrior II PA28-151 Manufacture’s Information Manual report: VB-573 Version 2, issued July 1973.


PRE FLIGHT

L Authorisation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETEMaintenance Release . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECTED AND SIGNEDPre flight Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS PER HANDBOOKBaggage . . . . . . . . . . . . . . . . . . . . . . . . . . . BAGGAGE AREA SECURE AND LOCKEDMandatory Documents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ABOARDTrip Sheet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOG START TIMEStart Position Suitable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SUITABLE

PRE START

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONCarb Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL COLDFuel Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DESIRED TANKThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ¼ INCH OPENMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKIF ENGINE DOES NOT START Within 10 sec PRIME AND REPEAT STARTINGPROCEDURE


Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ½ INCH OPENMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set 1000 RPMOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

AMD 7



FLOODED START

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPENMaster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT OFFStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETARDOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

POST START

Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

TAXYING

Brake Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKTurn Co-ordinator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSteering . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

PRE TAKE-OFF

Park Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2000 RPMMags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX DROP 175 RPM- MAX DIFF 50 RPMVacuum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Temp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKAnnunciator Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS TO TESTCarby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFFuel Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IDLEMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFlight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKFuel Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLEST TANKElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONEngine Gauges . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKCarby Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFSeat Backs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE & ERECTMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETBelts/ Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENEDEmpty Seats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SEAT BELTS SNUGLY FASTENEDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETTrim Tabs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL & FREE MOVEMENTDoors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LATCHED

L Engine Is warm for take off when throttle can be opened without engine faltering.

AMD 4


L Page 49PIPER PA28-151

LINE UP

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHFuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONDG & Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ALT ON

AFTER TAKE OFF

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPTrim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF/ CHECK PRESSUREOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil Temp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

PRE LANDING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKUndercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWNMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULLEST TANKOil Ts &Ps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKHarness & Hatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

AFTER LANDING

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDBYStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

SHUTDOWN

Electric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMMags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUTOFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL ARFTMags . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMaster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECUREHarness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STOWEDDoors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

AMD 7


Page 50PA-38-112 PIPER TOMAHAWK

Pre flight inspections and emergency procedures as per Piper Tomahawk PA-38-112Manufacturer’s Information Manual report: 2126 issued January 20 1978.



Cabin doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED AND LATCHEDOverhead latch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEDSeats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUSTED AND LOCKEDSeatbelts & Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENEDCircuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INParking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

L Carburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OFFFuel Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DESIRED TANK

ENGINE START

STARTING ENGINE WHEN COLD

Prime . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDOn last priming stroke leave primer in out position.Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN ½ INCHMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEPrimer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH IN SLOWLY AFTER ENGINE STARTThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE SLIGHTLYOil pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKElectric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFFuel pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKPrimer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOCKED


Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CRACKEDMaster switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUSTOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKElectric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFFuel pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK



STARTING ENGINE WHEN FLOODED

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN FULLMaster switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT-OFFStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGEMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETARDOil pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKFuel pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

STARTING WITH EXTERNAL POWER SOURCE (OPTIONAL EQUIPMENT)

Master switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAll electrical equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFTerminals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONNECTExternal power plug . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSERT IN FUSELAGEMaster switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON — CHECK AMMETEROil pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

WARM-UP

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 800 TO 1200 RPM

TAXIING

Radios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONTaxi area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEARBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSteering . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

GROUND CHECK

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1800 RPMMagnetos . . . . . . . . . . . . . . . . . . . . . . . . . MAX DROP 175 RPM — MAX DIFF 50 RPMVacuum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5.0”Hg ± .1Oil temp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKOil pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

L Carburettor heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETARDMagnetos . . . . . . . . . . . . CHECK GROUNDING AT LOW RPM, THEN SET TO BOTH

AMD 7



BEFORE TAKEOFF

Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON Flight instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKFuel Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PROPER TANKMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETElectric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

L Carburettor heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFEngine gauges . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKStatic source . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMALSeats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURELY LATCHED IN TRACKSeat backs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ERECTBelts/harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENEDEmpty seat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SEAT BELT SNUGLY FASTENEDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETTrim tab . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREEDoors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED & LATCHEDOverhead latch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGED

TAKEOFF

NORMAL

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETTab . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETAccelerate to 53 KIASControl wheel . . . . . . . . . . . . . . BACK PRESSURE TO ROTATE TO CLIMB ATTITUDE

SHORT FIELD, OBSTACLE CLEARANCE

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 DEGREES (FIRST NOTCH)Accelerate to 53 KIASControl wheel . . . . . . . . . . . . . BACK PRESSURE TO ROTATE TO CLIMB ATTITUDEAccelerate to 61 KIAS until obstacle clearanceAccelerate to 70 KIAS after obstacle is clearedFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT SLOWLY

SHORT FIELD, NO OBSTACLE

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 DEGREES (FIRST NOTCH)Accelerate to 53 KIASControl wheel . . . . . . . . . . . . . . BACK PRESSURE TO ROTATE TO CLIMB ATTITUDEAfter breaking ground accelerate to best rate of climb speed 70 KIASFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT SLOWLY

AMD 4


L Page 53PA-38-112 PIPER TOMAHAWK

SOFT FIELD, OBSTACLE CLEARANCE

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 DEGREES (FIRST NOTCH)Accelerate and lift off nose gear as soon as possibleLift off at lowest possible airspeedAccelerate just above ground to 61 KIAS to climb past obstacle height Continue climbing while accelerating to best rate of climb speed, 70 KIASFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SLOWLY RETRACT

SOFT FIELD, NO OBSTACLE

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 DEGREES (FIRST NOTCH)Accelerate and lift nose gear as soon as possibleLift off at lowest possible airspeedAccelerate just above ground to best rate of climb speed, 70 KIASFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SLOWLY RETRACT

CLIMB

Best rate (flaps up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 KIASBest angle (flaps up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61 KIASElectrical fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF AT DESIRED ALTITUDE

CRUISING

Reference performance charts and Avco-Lycoming Operator’s Manual.Normal max power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75%Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET PER POWER TABLEMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST

APPROACH AND LANDING

Fuel selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PROPER TANKSeat backs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ERECTBelts/harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENElectric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET 89 KIAS MAXTrim to 70 KIASFinal approach speed Full flaps (Outboard flow strips installed) . . . . . . . . . . . . . . . . . . . . . . . . . . 62 KIAS Full flaps (Outboard and inboard flow strips installed) . . . . . . . . . . . . . . . 67 KIAS

AMD 4


L Page 54PA-38-112 PIPER TOMAHAWK

STOPPING ENGINE

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACTElectric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL AFTMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT-OFFMagnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMaster switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF PARKING

Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETControl Wheel Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURED WITH BELTSFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL UPWheel chocks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN PLACETie downs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

AMD 7



Page 55

COMMANDER 112

Pre flight inspections and emergency procedures as per Rockwell Commander 112

Manufactures Information Manual report: P/N M112002-1 issued January 10 1998.


PRE FLIGHT

Authorisation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE

L Maintenance Release . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECTED AND SIGNED

Pre flight inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS PER HANDBOOK

Baggage . . . . . . . . . . . . . . . . . . . . . . . . . . . BAGGAGE AREA SECURE AND LOCKED

Mandatory Documents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ABOARD

Trip Sheet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOG START TIME

Start Position . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SUITABLE


Exterior Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE

Emergency Locator Transmitter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARM

Seats, Seat Belts and Shoulder Harness . . . . . . . . . . . . . . . . . ADJUST AND SECURE

(Front seats in upright position for takeoff)

Fuel Selector Valve (Serial Numbers 126 thru 380) . . . . . . . . . . . . . . RIGHT OR LEFT

(fullest tank)

Fuel Selector Valve (Serial Numbers 381 and Subs) . . . . . . . . . . . . . . . . . . . . . BOTH

Avionics master Switch (Serial Numbers 381 and Subs) . . . . . . . . . . . . . . . . . . . BOTH

Radios and Electrical Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Cowl flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPEN

Landing Gear Control Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN

Landing Gear Emergency Extension Valve Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

AMD 4


L Page 56COMMANDER 112

STARTING ENGINE

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT OFFPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPMThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CRACKED 1/4 INCHAlternate Induction Air . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COLDMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON(Note: ALT side of master switch should be OFF, if external power is used)

Voltmeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKFuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON(Note: Verify by sound that auxiliary fuel pump operates)

Mixture . . . . . . . . . . . . . . . . . ADVANCE MOMENTARILY, then back to IDLE CUT OFFFuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFPropeller Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEARIgnition Switch . . . . . . . . . . . . . . . . . . . . . . . . START then to BOTH when engine starts(Note: Cranking should be limited to 30 seconds, and several minutes allowed betweencranking periods to permit the starter to cool)

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICH after engine startsThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 800 to 1000RPMOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK for indication within 30 secondsAlternator Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON(Note: The BATT switch should be left ON for alternator turn-on and stabilisation)

Ammeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK for charging indicationVoltmeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK for 13-16 volts

STARTING ENGINE - FLOODED START PROCEDURE

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT OFFPropeller Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPMThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPENAlternate Induction Air Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COLDMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON(Note: The ALT side of the master switch should be OFF if external power is used)

Propeller Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEARIgnition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START then to BOTH(Note: Cranking should be limited to 30 seconds. Allow at least five (5) minutes betweencranking periods to permit the starter to cool.)

AMD 4



L Page 57

COMMANDER 112

As engine fires:

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETARD

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICH

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 800 to 1000 RPM

Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK for indication within 30 seconds

Alternator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON and CHARGING

(Note: The BATT switch should be left ON for alternator turn-on and stabilisation)

Ammeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK for charging indication

Voltmeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK for 13-16 volts

BEFORE TAKEOFF


Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FREE AND CORRECT MOVEMENT

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CYCLE Check operation and symmetry

Avionics Master Switch . . . . . . . . . . . . . . . . . . . . . ON (Serial Numbers 381 and Subs)

Instruments and Radios . . . . . . . . . . . . . . . . . . . . . . . . CHECK ANS SET AS DESIRED

Fuel Selector Valve (Serial Numbers 126 thru 380) . . . RIGHT OR LEFT (fullest tank)

(Note: Use of BOTH position on Serial Numbers 126 thru 380 is not recommended in

flight due to potential fuel imbalance and spillage)

Fuel Selector Valve (Serial Numbers 381 and Subs) . . . . . . . . . . . . . . . . . . . . . . BOTH

Elevator and Rudder Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TAKEOFF SETTINGS

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2000 RPM

Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Make Magneto check at 2000 RPM, as follows:

1. Ignition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTH to R. Note RPM

2. Ignition Switch . . . . . . . . . . . . . . . . . . . . . . . BOTH. Allow time for plugs to clear

3. Ignition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L. Note RPM

4. Ignition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTH

(The RPM drop should not exceed 175RPM on either magneto or indicate greater than

a 50 RPM differential between magnetos.)

(Note: An absence of RPM drop may be an indication of faulty magneto grounding or

improper timing. If there is doubt concerning ignition system operation, RPM checks

at a leaner mixture setting or higher engine speed will usually confirm whether a

deficiency exists.

AMD 7



Page 58

COMMANDER 112

Full throttle checks on the ground are not recommended unless the pilot has a good

reason to suspect that the engine is not operating properly, or desires to adjust the

mixture for high altitude or hot weather conditions. If a full throttle run-up is necessary,

monitor oil temperature and cylinder head temperature gauges to maintain

temperatures within limits.)

Propeller Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CYCLE/RETURN TO HIGH RPM

Induction Air Heat Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . CYCLE/RETURN TO OFF

(Note: A slight reduction in engine RPM will indicate proper operation).

L Optional Suction Gauge . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (4.5 to 5.2 In. Hg.)

Alternate Static Source Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMAL

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IDLE SPEED 600 to 700 RPM

Cabin Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK LATCHED

(Note: Lower and aft cabin door latching should be confirmed by gently pulling the

forward edge of the metal door latches inward. If the latch free play observed, after

the door is pulled closed, is greater than approximately 1/4-inch, the door is not

properly latched. Also verity that the upper door latches are in the aft (CLOSE)

position prior to takeoff.)

TAKEOFF

(Note: The maximum demonstrated crosswind velocity is 19 Knots.)

Auxiliary Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON at start of takeoff roll


Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10 DEGREES

(Note: Flap extension settings of greater that 20 degrees are not recommended for

takeoff.)

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE AND 2700 RPM

(Note: Proper full throttle engine operation should be checked early in the takeoff roll.

Any significant indication of rough or sluggish engine response is reason to

discontinue the takeoff.

When takeoff must be made over a gravel surface, it is important that the throttle be

applied slowly. This will allow the aircraft to start rolling before a high RPM is

developed, and gravel or loose material will be blown back from the prop area instead

of being pulled into it.)

AMD 4



L Page 59

COMMANDER 112

Aircraft Attitude . . . . . . . . . . . . . . . . . . . . . LIFT NOSEWHEEL AT 60KTS (69 MPH) IAS

Climb speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80 KTS (92 MPH) IAS

Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT IN CLIMB

Wing Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT

(Note: Takeoffs preceded by a rapid taxi turn are not recommended with less than 9.5

gallons of fuel in the Tank if either LEFT or RIGHT tank is selected.

Landing gear retraction should be avoided until well clear of the runway, and after a

positive rate of climb has been established. On long runways, gear retraction should

be delayed until reaching a point over the runway where a gear down forced landing

on that runway could no longer be made. Before retraction of the landing gear, the

brakes may be applied momentarily to stop tire rotation. Completion of the landing

gear retraction cycle is indicated by all position lights being out.)

CLIMB

For cruise climb, establish a power configuration of 26 inches Hg. Manifold pressure of

full throttle (use lower of the two) and 2600 RPM, with an airspeed of approximately 85-90

Kts (98 to 104 MPH) IAS. Adjust cowl flaps to maintain engine temperature within limits.

For maximum climb, establish a power configuration of full throttle and 2700 RPM, with

an airspeed of approximately 80 to 90 Kts (92-104 MPH) IAS. Adjust cowl flaps to

maintain engine temperature within limits.

CRUISE

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Normal cruising is made between 65 percent and 75 percent power. Observe all engine

operations limitations.

For Maximum engine service life, cylinder head temperatures should be maintained below

435°F during high performance cruise operation and 400°F for economy cruise settings.

To obtain greater cruising range at a specified throttle setting, select the lowest engine

RPM in the green arc range on the tachometer that will give smooth engine operation.

AMD 4



L Page 60

COMMANDER 112

When changing power settings, it is advisable to always increase RPM (with the propeller

control) before increasing manifold pressure, and to reduce manifold pressure (with the

throttle) before reducing RPM. Always remain within the established operating limits and

operate throttle and propeller controls slowly and smoothly.

(Note: Do not exceed 24 In.Hg. manifold pressure when below 2400 RPM.)

Fuel injector impact ice, which may form under certain atmospheric conditions causing an

unexplained loss of power, can be removed by application of full induction heat. Upon

regaining the original power indication, return the induction air control to the COLD

position. Induction filter ice can also form, as indicated by a drop in manifold pressure.

Full induction heat should be applied in this situation to regain the original manifold

pressure indication.

Elevator and Rudder Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST as required

Mixture Control . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST Best Power or Best Economy

(Note: Best economy mixture is obtained by leaning to peak EGT. Best power mixture

is obtained by leaning to peak EGT then enriching the mixture to 150°F on the rich side

of peak EGT.)

Caution: Never lean to peak EGT unless the power setting is 75% MCP or less, except

momentarily to establish peak.

Cow flaps . . . . . . . . . . . . . . . . . . . . . . . . ADJUST Close above 130 KTS (150 MPH) IAS

Fuel Selector Valve (Serial Numbers 126 thru 380) . . . . . . . . . . . . . . . RIGHT or LEFT

as required to maintain lateral trim

Fuel Selector Valve (Serial Numbers 381 and Subs) . . . . . . . . . . . . . . . . . . . . . . . BOTH

(Note: If use of BOTH position of fuel selector valve results in uneven fuel feeding,

maintain lateral trim by selecting LEFT or RIGHT as required.

Auxiliary Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

AMD 4



L Page 61

COMMANDER 112

DESCENT

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . RICH/OR LEAN FOR SMOOTH OPERATION

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

Cow flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED ABOVE 130 KTS (150 MPH) IAS

(Note: Let-down should be initiated far enough in advance of the destination to allow a

gradual planned rate of descent at cruising speed. Rate of descent should be

approximately 500 FPM for passenger comfort, using sufficient power to maintain engine

temperatures.)

BEFORE LANDING

Seats, Seat Belts and Shoulder harness . . . . . . . . . . . . . . . . . . ADJUST AND SECURE

(front seats in upright position)

Landing Gear . . . . . . . . . . . . . . . . . . . . . . . EXTEND/BELOW 130 KTS (150 MPH) IAS

Mixture Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICH

Fuel Selector Valve (Serial Numbers 126 thru 380) . . . . . . . . . . . . . . . . LEFT or RIGHT

(fullest tank)

Fuel Selector Valve (Serial Numbers 381 and Subs) . . . . . . . . . . . . . . . . . . . . . . BOTH

Propeller Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPM

Wing Flaps . . . . . . . . . . . . . . . . . . . . . . AS DESIRED BELOW 109 KTS (125 MPH) IAS

UP TO 20 DEGREES MAY BE USED BELOW 130 KTS (150 MPH) IAS

(Note: Recommended instrument approach speed with 20 degree flaps is 80 to 85 KIAS.)

Elevator and Rudder Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST as necessary

Auxiliary Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

(Note: Landing gear extension may be verified by illumination of the three gear down

position lights and the absence of a gear warn light and bell when the throttle is reduced

below approximately 14 inches manifold pressure, or when wing flaps are extended 25

degrees or more regardless of power setting.)

GO-AROUND

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE AND 2700 RPM

Flaps . . . . . . . . . . . . . . RETRACT TO 0 DEGREES WHILE MAINTAINING ALTITUDE

Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT AFTER CLIMB IS ESTABLISHED

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPEN

AMD 7


Page 62COMMANDER 112

LANDING

(Note: The maximum demonstrated crosswind velocity is 19 knots.)

Airspeed on Final . . . . . . . . . . . . . . . . . . . . . . . . . . . 73 KTS (84 MPH) IAS with full flapsL Touchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRST

Landing Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOWER NOSE WHEEL GENTLYBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MINIMUM REQUIREDCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPENWing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT after clearing runwayAuxiliary Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF after clearing runway

SECURING THE AIRCRAFT

Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET'Avionics Master Switch (Serial Numbers 381 and Subs) . . . . . . . . . . . . . . . . . . . . . OFFRadios and Electrical Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUTOFFIgnition and Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFControl Wheel Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSTALLEDFuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFParking Brake . . . . . . . . . . . . . . . . . . . . . . RELEASE AND INSTALL WHEEL CHOCKSControl Locks, Tie Downs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSTALL

COLD WEATHER OPERATIONS

The starting procedure for cold weather operation is basically the same as that presentedin the Normal Procedures.

Warning: Before performing the External Inspection, remove any accumulations of frost,ice or snow from wings, tail and all flight control surfaces.

Warning: Before pulling a propeller through by hand, check ignition switch OFF, andvisually check the security of magneto ground wire attachment to prevent inadvertentengine firing.

In extremely cold weather, the use of external preheaters and the availability of anexternal power unit (if your aircraft is equipped with the optional ground servicereceptacle) are recommended to reduce wear and abuse to the engine and to conservebattery energy. Also, caution should be exercised to prevent inadvertent forwardmovement of the aircraft when started on icy or snow-packed surfaces. The position ofthe Master Switch is important in starting operations using external power. Beforeconnecting external power to the aircraft, the BATT half of the split master Switch shouldbe turned ON, and the ALT portion of the Master Switch left OFF. After the engine hasstarted, disconnect the external power. The Alt half of the Master Switch should then beturned ON to allow normal electrical system charging.

AMD 5


Page 63BEECHCRAFT BONANZA 36, A36

Pre flight inspections and emergency procedures as per Beechcraft Bonanza 36, A36Manufactures Information Manual P/N36-590002-19C3 issued July 1994.


PRE FLIGHT

Authorisation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETEMaintenance Release . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECTED AND SIGNEDPre flight inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS PER HANDBOOKBaggage . . . . . . . . . . . . . . . . . . . . . . . . . . . BAGGAGE AREA SECURE AND LOCKEDMandatory Documents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ABOARDTrip Sheet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOG START TIMEStart Position . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SUITABLE

PRE START

Seats/Seat Backs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . POSITION &LOCKSeat Belts & Shoulder Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENParking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETAll Avionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFCircuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INLanding Gear Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWNFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENLight Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDFuel Selector Valve . . . CHECK OPERATION, SELECT TANK MORE NEARLY FULLBattery & Alternator Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFuel Quantity Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK QUANTITY

WARNING

DO NOT TAKE OFF IF GAUGES INDICATE IN YELLOW ARCOR WITH LESS THAN 13 GALLONS IN EACH MAIN TANK

STARTING

CAUTION

VERNIER-TYPE ENGINE CONTROLS SHOULD NOT BEROTATED CLOCKWISE AFTER BEING ADVANCED

TO THE FULL

AMD 5



Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPMThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPENAuxiliary Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . ON until fuel flow peaks then OFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Approximately 1/4 inch openMagneto/Start Switch . . START position, release to BOTH position when engine fires

CAUTION

DO NOT ENGAGE STARTER FOR MORE THAN 30 SECONDS IN ANY 4MINUTE TIME PERIOD

In the event of an over prime conditionMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT-OFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENMagneto/Start Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START PositionAs engine fires reduce throttle to IDLE and advance the mixture control to FULL RICH

NOTE - During hot starts the auxiliary fuel pump is turned on momentarily after startingto purge system, then turned off

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 to 1200RPMOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKAlternator Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON, check for chargingAll Engine Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

CAUTION

The ammeter indication should be less than 25% of full chargeat1000 to 1200 RPM within two minutes, with no additionalelectrical equipment on. If not, turn off battery and alternatorswitches, and do not take off.

AFTER STARTING AND TAXI

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE & CHECKAvionics Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON, AS REQUIREDLights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

CAUTION

DO NOT OPERATE ENGINE ABOVE 1200 RPM UNTIL OILTEMPERATURE REACHES 75° F (24° C)

AMD 5



BEFORE TAKE OFF

Seat Belts & Should Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

NOTE

ALL RECLINING SEATS MUST BE IN THE UPRIGHTPOSITION DURING TAKE OFF

Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEngine Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKFlight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK & SETAmmeter . . . . . . . . . . . CHECK for stabilised indication between 0 & 25% of full charge at 1000 to 1200 RPMAuxiliary Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK OFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1700 RPMPropeller . . . . . . . . . . . . . . . EXERCISE to obtain approximately 300 to 400 RPM drop, return to high RPMMagnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK at 1700 RPM(variance between individual magnetos should not exceed 50 RPM, max drop not toexceed 150 RPM)Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

(Aileron - NEUTRAL)(Elevator 3E (6E nose up if only front seats are occupied))

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPDoor &Windows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECUREControls . . . . . . . . . . . . . CHECK PROPER DIRECTION & FREEDOM OF MOVEMENTMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICH (or as req by field elevation)Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASEDInstruments . . . . . . CHECK (Make final check of manifold pressure, fuel flow and RPM

at the start of the take-off run)

TAKE OFF

Take off power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE 2700 RPMPower . . . . . . . SET TAKE OFF POWER (Mixture - SET as required by field elevation)Brakes . . . . . . . . . . . . . . . . . RELEASE THEN ACCELERATE to recommended speedsLanding Gear . . . . . . . . . . . . . . . RETRACT (when positive rate of climb is established

and insufficient runway remains for landing)Airspeed . . . . . . . . . . ESTABLISH DESIRED CLIMB SPEED (when clear of obstacles)

AMD 5



CLIMB

Maximum Continuous . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLECruise Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25in HG (or full throttle) 2500 RPMEngine Temperatures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITORPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET AS DESIREDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET FUEL FLOW

CRUISE

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSEDPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET FUEL FLOW

DESCENT

Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETCowl Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSEDPower . . . . . . . . . . . . . . . . AS REQUIRED (avoid prolonged idle settings & low CHTs)Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENRICH AS REQUIRED

BEFORE LANDING

Seat Belts & Shoulder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURENOTE - All reclining seats must be in the upright position during landing

Fuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . SELECT TANK MORE NEARLY FULLCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICH (or as required by field elevation)Landing (Dear . . . . . . . . . . . . . . . . . DOWN & CHECK (observe max extension speed)Landing and Taxi Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN (observe max extension speed)Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . ESTABLISH LANDING APPROACH SPEEDPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPM

AFTER LANDING

Landing and Taxi lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPTrim Tab . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET TO 0ECowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

AMD 5



SHUTDOWN

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETElectrical & Radio Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSEMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT-OFFMagneto Start Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF after engine stops

Battery and Alternator Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFControl Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSTALL, if conditions warrantInstall wheel chocks and release brakes if the aeroplane is to be left unattended.

AMD 5


Page 68


AMD 6


Page 69DE HAVILLAND TIGER MOTH DH-82A

Pre flight inspections and emergency procedures as per The De Havilland Tiger MothMaintenance Manual issued June 1947 and DH-Gypsy Major Aero Engine Care andMaintenance Manual (1st Australian Edition).


PRIOR TO ENTERING AND ON ENTERING THE COCKPIT

1. (a) Check fuel and oil contents.(b) See that magneto switches are OFF.(c) See that doors and harnesses are secure. If flying solo, see that front harness

is secured so that it cannot interfere with controls and that the column hasbeen removed and stowed in luggage locker. If flying with passenger, checkearphones.

(d) Set altimeter to zero feet.(e) Wind clock, check and note time.(f) Ensure that compass grid ring rotates freely and that the clamp functions.(g) Operate controls and see that surfaces move freely and in correct sense.(h) If locking gear is fitted, unlock slats, set tail trimmer back for taxying.

STARTING ENGINE AND GROUND CHECK

2. (a) Set throttle in closed position.(b) Put fuel cock fully ON.

AMD 6


Page 70

(c) Switch ON front magneto switch, on receipt of"CONTACT" from ground engineer.

(d) Switch ON rear magneto switch when engine is running.(e) Warm engine for 4 minutes at 800 rpm with 30psi minimum oil pressure.(f) Check for magneto drop, by running engine at 1500rpm and switching off each

magneto in turn. The drop in rpm should not exceed 50.(g) Run engine at full throttle for 10 seconds (1900 - 2100rpm) at which the

minimum oil pressure should be 30psi.(h) Slacken throttle friction nut for taxying.

TAXYING3. (a) Hold the control column well back (except when taxying downwind), to keep

the tail on the ground and increase the effectiveness of the rudder control.Short bursts of throttle are necessary for turning purposes; brakes are notfitted.

(b) The forward view from the cockpits on the ground is restricted and a zigzagcourse should be steered to see the path ahead is clear.

TAKE OFF

4. (a) Set trimmer control two-thirds forward.(b) Tighten throttle friction nut.(c) Set mixture control at RICH (BACK). (d) See that the slats are unlocked (if locking gear is fitted).(e) Check oil pressure; approximately 40psiminimum 30psi.

AMD 6


Page 71

There is a tendency for the aircraft to swing to the right during take-off, due to the torqueeffect, which is corrected, easily, by applying rudder as the throttle is opened.

PERFORMANCE at 1650lbs, 749kgs

5. Indicated stalling speed - 39 knotsNormal climbing and gliding speed - 56 kts at2100rpmNormal cruising speed - 74 - 78 knots at 1900 - 2000 rpmMaximum speed at sea level - 91 - 95 knotsRate of climb at sea level - 800 ft per minuteService ceiling (100fpm rate of climb) - 15,800 ft

GLIDING

6. (a) Set trimmer back or within 1 or 2 notches from the end.(b) Check that slats are unlocked if locking gear is fitted; these may have been

locked during the course of the flight for the performance of aerobatics.(c) If descending from a considerable altitude, give occasional bursts of throttle

to warm engine.

AFTER LANDING

7, (a) Set trimmer fully back.(b) Slacken throttle friction nut.(c) Lock slats.(d) Turn fuel OFF.(e) Switch OFF magneto when engine falters

AMD 6


Page 72FUEL CONSUMPTION

8. (a) 30L per hr at 2000rpm.

EMERGENCIES

9 - Fire Appliance(a) A fire extinguisher is fitted in each of the cockpits and is readily accessible

from inside and outside the cockpit.(b) It is detached by pulling lifting spring clamp and removing from bracket.

First Aid(a) A first aid kit is carried in the luggage compartment.

Abandoning the Aircraft(a) The captain should order the other occupant to leave first.(b) Both occupants should use the following procedure:

Open cockpit doorDisconnect intercommunication lead and undo safety harnessSlide over the side, head foremost and facing the tail.

AMD 8



Page 73

L CESSNA MODEL 182

Pre flight inspections and emergency procedures as per Cessna Model Cessna 182Manufacturers Information Manual D1176-13 (RGI-110-8/03) issued October 1979.


PRE FLIGHT


PRE START

Seats/Seat Backs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . POSITION &LOCKSeat Belts & Shoulder Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENFuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTHAll Avionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST & SETCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENCircuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IN

STARTING

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPMCarburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COLDThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN ½ INCHPrime . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONPropeller Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEARIgnition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START (release when engine starts)

NOTEIf engine has been overprimed, start with throttle ¼ to ½ inch open. Reduce throttle toidle when engine fires.

POST START

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKFlashing Beacon and Navigation Lights . . . . . . . . . . . . . . . . . . . . . . . . . ON as requiredAmmeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKRadios & Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

AMD 8



Page 74

L CESSNA MODEL 182

TAXI

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKINGGyro Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

BEFORE TAKE OFF

Cabin Doors and Windows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..CLOSED & LOCKEDParking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETFlight Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREE & CORRECTFlight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETFuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTHMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHElevator & Rudder Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TAKEOFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1700RPMMag Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

(RPM drop < 150 RPM; Differential < 50 RPM)Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CYCLECarburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEngine Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKAmmeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSuction Gauge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 800 – 1000RPMRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETAutopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFThrottle Friction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FIRMParking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE

LINE UP

Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONDG/Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

TAKE OFF

Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0E – 20ECarburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COLDPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE & 2400 RPMElevator Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LIFT NOSE WHEEL at 50 KIASClimb Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 KIAS (flaps 20E)

80 KIAS (flaps UP)Airspeed . . . . . . . . . . ESTABLISH DESIRED CLIMB SPEED (when clear of obstacles)

AMD 8


Page 75L CESSNA MODEL 182

SHORT FIELD TAKEOFF

Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20ECarburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COLDBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLYPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE and 2400 RPMBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASEElevator Control . . . . . . . . . . . . . . . . . . . . MAINTAIN SLIGHTLY TAIL LOW ATTITUDEClimb Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 57 KIAS

(until all obstacles are cleared)Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT slowly after reaching 70 KIAS

NORMAL CLIMB

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 85 – 95 KIASPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23 INCHES Hg & 2400 RPMFuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTHMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICHCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

CRUISE

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15 – 23 INCHES; 2100 – 2400 RPM(no more than 75% power)

Elevator and Rudder Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUSTMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEANCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

DESCENT

Fuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTHPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIREDCarburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL HEAT AS REQUIREDMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENRICHEN AS REQUIREDCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSEDWing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

(0 – 10E below 140 KIAS, 10E – 40E below 95 KIAS)

BEFORE LANDING

Seats, Belts & Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST & LOCKFuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTHMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHCarburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPMAutopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

AMD 8



Page 76

L CESSNA MODEL 182

NORMAL LANDING

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 – 80 KIAS (flaps UP)

Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

(0 – 10E below 140 KIAS, 10E – 40E below 95 KIAS)

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 60 – 70 KIAS (flaps DOWN)

Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST

Touchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRST

Landing Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOWER NOSE WHEEL GENTLY

Braking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MINIMUM REQUIRED

AFTER LANDING

Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Carburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COLD

Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT to 20ECowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

SHUTDOWN

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Electrical & Radio Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSE

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT-OFF

Ignition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF after engine stops

Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Control Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSTALL

Fuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RIGHT

AMD 9



Page 77L PARTENAVIA PN68

NORMAL PROCEDURES

PRE STARTPre-Flight Checks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETEPassenger Brief . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETESeat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUSTED & LOCKEDHatches & Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECUREControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREE & CORRECTCircuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAlternate Air . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFTrims . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON MAINSMaster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONAlternator Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMagnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

START AND AFTER STARTLEFT ENGINEMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHPitch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL FINEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HALF / PRIMEMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT OFFThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETClear Prop & Press Starter 3 SECONDSIdle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMAlternator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON (CHECK LOAD)Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN THE GREENSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SOURCE FUNCTIONINGRIGHT ENGINE - SAME PROCEDURE

BEFORE TAXIAvionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONHF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREQUENCY SELECTED & CHECKEDVHF Nav . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . / SET / IDENTIFIED/TESTEDADF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TUNED / IDENTIFIED/TESTEDDME . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TUNED / IDENTIFIED/TESTEDDirectional Gyro . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETVHF Coms . . . . . . . . . . . . . . . . . . . . . . . . . CLEARANCE - SET TRANSPONDER CODE

SET ASSIGNED ALTITUDE INDICATORATIS SET QNH & HDG BUG FOR DUTY RWYTAXY CALL

AMD 9




TAXY CHECKSFlight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMAL

PRE TAKE OFFEngine Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ALL IN GREENRun Up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2300 PITCH

1900 MAGS (MAX DROP 125)1500 FEATHER (300 DROP)

Vacuum Gauge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDAlternators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & CHARGINGIdle RPM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check SET 1000 RPMTrims . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET FOR TAKE OFFMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHPitch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL FINEMagnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ALL SWITCHES ONFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15EFriction Nut . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON POSITION

QUANTITY SUFFICIENTInstruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED /SETSwitches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK LEFT TO RIGHTNav Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET FOR DEPARTUREControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL & FREEHatches / Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

PRE TAKE OFF CONSIDERATIONS90 Kts = BEST SEROCSEROC PERFORMANCETERRAIN/OBSTACLESTAKE OFF MINIMATAKE OFF INTENTIONSSID/DEPARTURE PROCEDURESRADIO CALL

LINE UPFuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONPitot Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON (IF ENTERING CLOUD)Strobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON/ALT

AMD 9



AFTER TAKE OFFBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY /RELEASEGear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FIXEDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25" / 2500 RPMEngine Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN THE GREENFuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF / FUEL FLOWS STABLE

TOP OF CLIMBCruise Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23" / 2400 RPMMixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEANEDDirectional Gyro . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET TO COMPASSAltimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET AREA QNHFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . QUANTITIES NOTEDPosition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTED

CRUISERevise ETAPlan Descent Point

APPROACH BRIEFSelf Brief . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FAMILIARISE ALL SEGMENTSTAF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RUNWAY TO USE

ORIENTATION OF RUNWAYTOP OF DESCENTTraffic . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTEDLowest Safe Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETDestination QNH . . . . . . . . . . . . . . . . . . . . . . . . . . SET / ALTIMETERS CROSS CHECKMixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHEN AS REQUIREDFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON MAINS

APPROACHING DESTINATIONNav Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET FOR APPROACHSlowed Down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18" / 2400 RPM / FLAPS 15E Ident . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOREDSelf Brief . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK SECTOR ENTRYTAF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK WIND DIRECTION

INSTRUMENT APPROACH SPEEDSHolding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18" / 2400 RPMInitial Leg If Descending . . . . . . . . . . . . . . . . . . . . . . . . . 15" / 2400 RPM / GEAR DOWNFinal Leg for Circling . . . . . . . . . . . . . . . . . . . . . . . . . . . 18" / 2400 RPM / GEAR DOWNFinal Leg for Runway Approach . . . . . . . . 18" / 2400 RPM / GEAR DOWN / FLAPS 15E

AMD 9




PRE LANDINGBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF / PRESSURE CHECKEDUndercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FIXEDMixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHFuel / Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON & SUFFICIENTHatches / Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

NORMAL LANDINGBase . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15E FLAPS/ TO GIVE 110 KTS -100 KTS

FINAL APPROACHPitch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL FINEUndercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FIXEDFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 35ETO GIVE 90 KTS - 85 KTSFlaps (Cowl) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOT APPLICABLE

AFTER LANDINGPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMTransponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF Trims . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NEUTRALFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFuel Booster Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFPitot Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFStrobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFExternal Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIREDRadio . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CALL AS NECESSARY

SHUTDOWNPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPMMagnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKSwitches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAvionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFEngine Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN THE GREENMixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT OFFThrottles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSEDMagnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF Alternator Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMaster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOCKED

AMD 9





ENGINE FAILURE - TAKE OFFBelow decision speed (must be at least 90kts)Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSE AND LAND AHEAD

Above decision speedControl . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAIN Mix . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPitch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPGear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPIdentify . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DEAD LEG DEAD ENGINE

CONFIRMFEATHER

Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . at VYSE of 90kts (blue line)

When time permits, secure engine as follows:Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ICOThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSEDFuel boost pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFFuel selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMagnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAlternator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFElectric load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR

Engine Failure In CruiseControl . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAINTAINMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPitch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPGear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Identify re-identify and featherMixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKEDFuel selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONBoost pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMagnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKED L & R

If power not restored, proceed to shut down the engine.Failed Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SHUTDOWN

AMD 9



ENGINE FIRE IN FLIGHTFuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEANThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSEDFuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFIf fire not outGear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWNFlap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWNAircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LAND

OR If fire goes out.Mixture on live engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPitch on live engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPPower on live engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPGear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFlap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPFailed Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IdentifyPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FeatherFailed Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Shutdown

EMERGENCY DESCENTThrottles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTH CLOSEDFlap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full Descent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AT 101 ktsNote: Medium turns during descent will significantly increase rate of descent.

ELECTRICAL FAILURES

One Alternator Off LineInop. alternator switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFCircuit breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECKInop. alternator switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON* If power not restored (Alt OFF), reduce electrical load to a maximum of 50 amps.

Both Alternators Off LineTry to restore operation as per one alternator off-line. If not successful:Battery master switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAlternator switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON (One at a time)

If operation not restored:Battery master switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONAlternator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFNote: Battery power only is available and will last for approx 20 mins.

AMD 11



Page 83

L SUPER DECATHLON 8KCAB

Operating checklist and emergency procedures as per Flight Operations Manual

(08APR2005) for Super Decathlon model 8KCAB.


PRE FLIGHT


Maintenance Release . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECTED AND SIGNED


Baggage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE AND LOCKED




PRE START

Seat belts/shoulder harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENED

Fuel shut-off valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Electrical switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Cabin door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

Flight Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Radio . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

AMD 11



Page 84


STARTING

Cabin door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Seats belts & harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENED or STOWED


Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Propeller control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL INCREASE

Alternate air . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COLD

Electrical & radio switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Master switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Engine prime . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

a. Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICH

b. Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1/4 TO 1/2 INCH OPEN

c. Electric fuel pump . . . . . . . . . . . . . . . . ON until pressure indicated, then OFF

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT-OFF

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1/2 to 1 INCH OPEN

Magneto switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTH ON

Propeller & blast area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Starter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGE

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICH

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 to 1200 RPM

Oil pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Electrical & radio switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

The amount of fuel priming will vary with each engine and temperature condition. If the

engine is warm, little or no prime is required.

AMD 11



Page 85


TAXI

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKING

Gyro instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

BEFORE TAKE-OFF

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Flight Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREE AND CORRECT

Elevator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Flight Instruments/Radio . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK AND SET

Master switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Fuel shut-off value . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON


Engine Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Engine Run-Up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1800 RPM

Magnetos . . . . . . . . . . . . . . . . . . . CHECK (175 RPM MAX DROP, 50 RPM MAX DIFF)

Propeller . . . . . . . . . . . . . . . . . . . . . . CHECK (full decrease until RPM drop of 300-500)

Alternate air . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COLD


Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

Electric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Cabin doors & windows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED and LATCHED

Seat belts & shoulder harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENED

TAKE-OFF

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPEN


Attitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RAISE TAIL

Lift Off . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55-60 MPH

Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75-80 MPH

AMD 11



Page 86


CLIMB


Propeller Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL INCREASE

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75-80 MPH

Electric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

CRUISE

Level-off . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TRIM

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ACCELERATE TO CRUISE SPEED

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET RPM

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN

DESCENT


Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

LANDING

Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENED

Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL INCREASE

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

Electric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FIRM (PARK BRAKE OFF)

Approach Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70-75 MPH

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED TO CONTROL GLIDE PATH

After touchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . POWER OFF, BRAKE

Electric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

AMD 11



Page 87


SHUTDOWN

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Electrical Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF


Magnetos/Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Wheels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHOCKED

Wing/Tail tie downs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

AMD 11



Page 88


AMD 12



Page 89

CESSNA 310R

LPre flight inspections and emergency procedures as per Cessna Model 310R Airplane

Flight Manual D1528R4-13, Revision 4, dated 2nd April 1982.

AIRSPEED FOR SAFE OPERATION

Conditions:

1. Takeoff Weight 5500 Pounds

2. Landing Weight 5400 Pounds

3. Sea Level, Standard Day

(1) Takeoff and Climb to 50 Feet (0E Flaps) . . . . . . . . . . . . . . . . . . . . . . . . 92 KIAS

(2) All Engines Best Angle-of-Climb Speed . . . . . . . . . . . . . . . . . . . . . . . . . 85 KIAS

(3) All Engines Best Rate-of-Climb Speed . . . . . . . . . . . . . . . . . . . . . . . . . 107 KIAS

(4) All Engines Landing Approach Speed (35E Flaps) . . . . . . . . . . . . . . . . . 93 KIAS

(5) manoeuvring Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 148 KIAS

(6) Structural Cruise Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 181 KIAS

(7) Never Exceed Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 223 KIAS

(8) Speed for Transition to Balked Landing Conditions . . . . . . . . . . . . . . . . 85 KIAS

(9) Maximum Demonstrated Crosswind Velocity . . . . . . . . . . . . . . . . . . . 19 KNOTS

AMD 11



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L CESSNA 310R

BEFORE ENGINE STARTING

1. Preflight Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE

2. Control Lock(s) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE

3. Seat, Seat Belts and Shoulder Harness . . . . . . . . . . . . . . . ADJUST and SECURE

4. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST and SET

5. Landing Gear Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN

6. Emergency Alternator Field Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

7. Emergency Avionics Power Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

8. Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN

9. All Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

10. Avionics Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

11. Auxiliary Fuel Pump Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

12. Battery and Alternators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

13. Lighting Rheostats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

14. Altimeter and Clock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

15. All Warning Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS-TO-TEST

16. Landing Gear Position Indicator Lights . . . . . . . . . . . . . . . . Check green lights ON

17. Cabin Air Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

18. Fuel Quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

19. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN ONE INCH

20. Propellers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL FORWARD

21. Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICH

22. Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOCKED FULL OPENS

23. Fuel Selectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAIN TANKS (Feel For Detent)

24. Alternate Air Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN

25. Anti-Collision Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

AMD 11



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L CESSNA 310R

ENGINES STARTING (Left Engine First Without External Power)

1. Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

2. Magneto Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

3. Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START

a. Starter Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS

b. Primer Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Left Engine - LEFT

Right Engine - RIGHT

4. Auxiliary Fuel Pump . . . . . . . . . . . . . . . . . . . LOW to purge vapour from fuel system

5. Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 800 to 1000 RPM

6. Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

7. Right Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START. Repeat steps 1 through 6

8. Alternators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

ENGINES STARTING (Left Engine First With External Power)

1. Battery and Alternators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

2. External Power Source . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ATTACH

3. Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

4. Magneto Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

5. Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START

a. Starter Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS

b. Primer Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Left Engine - LEFT

Right Engine - RIGHT

6. Auxiliary Fuel Pump . . . . . . . . . . . . . . . . . . . LOW to purge vapour from fuel system

7. Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 800 to 1000 RPM

8. Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

9. Right Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START. Repeat steps 3 through 8

10. External Power Source . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVE

11. Battery and Alternators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

12. Alternators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

AMD 11



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L CESSNA 310R

BEFORE TAXIING

1. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

2. Avionics Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

3. Avionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

4. Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

5. Cabin Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

a. If heating and defrosting is required:

(1) Cabin Air Knobs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

(2) Defrost Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

(3) Temperature Control Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

(4) Cabin Heat Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HEAT

(5) Heat Registers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

b. If ventilation is required:

(1) Cabin Air Knobs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

(2) Cabin Heat Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FAN

(3) Heat Registers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

6. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE

TAXIING

1. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

2. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

3. Rate Gyros . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

AMD 11



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L CESSNA 310R

BEFORE TAKEOFF

1. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

2. Engine Runup:

a. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1700 RPM

b. Alternators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

c. Vacuum System . . . . . . . . . . . . . . . . . . . . . . . . . CHECK 4.75 to 5.25 inches Hg

d. Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK 150 RPM

maximum drop with a maximum differential of 50 RPM

e. Propellers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK feathering to 1200 RPM;

return to high RPM

f. Engine Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK green arc

g. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

3. Flight Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK, free and correct

4. Trim Tabs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

5. Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOCKED FULL OPEN

6. Alternate Air Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN

7. Fuel Selectors . . . . . . . . . . . . . . . . . . . . . . . RECHECK - Left Engine - LEFT MAIN

(Feel For Detent)

Right Engine - RIGHT MAIN

(Feel For Detent)

8. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

9. Cabin Door and Window . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED and LOCKED

10. Fuel Quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

11. Flight Instruments and Avionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

12. Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

13. Auxiliary Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOW

14. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE

15. Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

AMD 11



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L CESSNA 310R

TAKEOFF

NORMAL TAKEOFF

1. Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE and 2700 RPM

2. Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN for field elevation (See Figure 5-27)

3. Air Minimum Control Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80 KIAS

4. Elevator Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Raise nosewheel at 83 KIAS

5. Lift-Off . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 92 KIAS

MAXIMUM PERFORMANCE TAKEOFF

1. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN 15E2. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

3. Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL THROTTLE

4. Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN for field elevation (See Figure 5-27)

5. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE

6. Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK 2700 RPM

7. Elevator Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Raise nosewheel at 70 KIAS

8. Air Minimum Control Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80 KIAS

9. Lift-Off . . . . . . . . . . . . . . . . . . . 82 KIAS. Hold speed until all obstacles are cleared

AFTER TAKEOFF

1. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY momentarily

2. Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT. Check red light OFF

3. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

4. Climb Speed . . . . . . . . . . . . . . . 107 KIAS (All Engines Best Rate-Of-Climb Speed)

5. Auxiliary Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

AMD 11



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L CESSNA 310R

CLIMB

CRUISE CLIMB

1. Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2500 RPM and 24.5 inches Hg

2. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 115 to 130 KIAS

3. Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST to climb fuel flow

4. Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN or as required

5. Auxiliary Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . LOW above 12,000 feet altitude

to minimise vapour formation

6. Propellers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SYNCHRONISE manually

7. Quadrant Friction Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TIGHTEN securely

(With Synchrophaser Installed)

8. Propeller Synchrophaser . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SYNC

(Optional System)

MAXIMUM CLIMB

1. Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2700 RPM and FULL THROTTLE

2. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 107 KIAS at sea level

99 KIAS at 10,000 feet

3. Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST for altitude and power

4. Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN or as required

5. Auxiliary Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . ON above 12,000 feet altitude

to minimise vapour formation

AMD 11



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L CESSNA 310R

CRUISE

1. Cruise Power . . . . . . . . . . . . . . . . . . 2100 to 2500 RPM and 15.0 to 24.5 inches Hg

2. Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN

Recheck if power, altitude or OAT changes

3. Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN or as required

4. Propellers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SYNCHRONISE manually

5. Quadrant Friction Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TIGHTEN securely

(With Synchrophaser Installed)

6. Propeller Synchrophaser . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SYNC

(Optional System)

7. In Smooth Air After Propellers Synchronise . . . . . . . . . . . . . . . . . . . . . . . . . PHASE

Phasing Knob ADJUST for desired phasing position (Optional System)

8. Auxiliary Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . LOW when switching tanks

9. Fuel Selectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Left Engine - LEFT MAIN

(Feel For Detent)


(Feel For Detent)

a. If optional 40-gallon auxiliary tanks are installed,

Fuel Selectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAIN TANKS for 60 minutes

b. If optional 63-gallon auxiliary tanks are installed,

Fuel Selectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAIN TANKS for 90 minutes

c. Usable auxiliary fuel quantity is based on level flight

d. If wing locker tanks are installed, fuel selectors

MAIN TANKS or, after wing locker tanks are transferred and main tank quantity

is less than 180 pounds each - AUXILIARY TANKS

e. If wing locker tanks are installed,

Crossfeed - SELECT as required to maintain fuel balance after wing locker tank

fuel transfer

10. If oxygen use is desired, proceed as follows:

a. Mask . . . . . . . . . . . . . . . . . . Connect mask and hose assembly and put mask on

b. Hose Coupling . . . . . . . . . . . . . Plug into oxygen outlet in the overhead console

c. Oxygen Flow Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check Flow

(Indicator Toward Mask Indicates Proper Flow)

d. Disconnect hose coupling when not in use

11. Trim Tabs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST

AMD 11



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L CESSNA 310R

DESCENT

I. Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

to maintain engine temperatures in the green

2. Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

3. Propeller Synchrophaser . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

(Optional System)

4. Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST for smooth operation

with gradual enrichment as altitude is lost

5. Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

BEFORE LANDING

1. Fuel Selectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Left Engine - LEFT MAIN

(Feel For Detent)


(Feel For Detent)

2. Auxiliary Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOW

3. Alternate Air Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IN

4. Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED for flight altitude

5. Propeller Synchrophaser . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

(Optional System)

6. Propellers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL FORWARD

7. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN 15E below 158 KIAS

8. Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN below 138 KIAS

9. Landing Gear Position Indicator Lights . . . . . . . . . . . . . . . . . Check down lights ON;

Unlocked Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

10. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN 35E below 138 KIAS

11. Minimum Multi-Engine Approach Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . 93 KIAS

12. Air Minimum Control Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80 KIAS

AMD 11



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L CESSNA 310R

BALKED LANDING

1. Increase engine speed to 2700 RPM and apply full throttle if necessary

2. Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

3. Balked Landing Transition Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 85 KIAS

4. Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . during IFR go-around or simulated IFR go-around

5. Wing Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE setting to 15E6. Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TRIM for climb

7. Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

8. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT

as soon as all obstacles are cleared and a safe altitude and airspeed are obtained

AFTER LANDING

1. Auxiliary Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOW during landing roll

2. Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

3. Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

SHUTDOWN

1. Auxiliary Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

2. Avionics Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

3. All Switches Except Battery, Alternator and Magneto Switches . . . . . . . . . . . . OFF

4. Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE

5. Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT-OFF

6. Magneto Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF, after engines stop

7. Battery and Alternators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

8. Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

9. Control Lock(s) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSTALL

10. Fuel Selectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

if a long period of inactivity is anticipated (Feel For Detent)

11. Cabin Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSE

AMD 11



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L CITABRIA 7GCAA

Operating checklist and emergency procedures as per Flight Operations Manual for

Citabria model 7GCAA.

Document: American Champion Aircraft FAA Approved Aeroplane Flight Manual Citabria

Adventurer model 7GCAA, Serial Nos 400-97 and up.


PRE-FLIGHT


Maintenance Release . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECTED AND SIGNED


Baggage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE AND LOCKED




PRE START

Seat belts/shoulder harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENED


Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Electrical switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Cabin door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

STARTING

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FUEL RICH

Gas . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Prime . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS NECESSARY

Master . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Ignition switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN 1/4 TO 1/2 INCH

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Starter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGE

Do not operate starter continuously for more than 15 seconds. If no oil pressure 30

seconds after start, stop engine and determine cause.

AMD 11



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L CITABRIA 7GCAA

TAXI

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKING

Gyro instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

BEFORE TAKE-OFF

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Flight Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREE AND CORRECT

Elevator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Flight Instruments/Radio . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK AND SET

Fuel shut-off value . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON



Engine Run-Up . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1800 RPM

Magnetos . . . . . . . . . . . . . . . . . . . CHECK (200 RPM MAX DROP, 50 RPM MAX DIFF)

Carburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK THEN COLD


Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

TAKE-OFF



Attitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RAISE TAIL

Lift Off . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 55-60 MPH

Climb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75-80 MPH

AMD 11



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L CITABRIA 7GCAA

CLIMB


Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICH (BELOW 5000FT)

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75-80 MPH

CRUISE

Level-off . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TRIM

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ACCELERATE TO CRUISE SPEED

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET RPM

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN

DESCENT


Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

LANDING

Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENED

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FIRM (PARK BRAKE OFF)

Approach Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 60-70 MPH

Throttle . . . . . . . . . . . . . . . . . . . . . . AS DESIRED TO CONTROL RATE OF DESCENT

SHUTDOWN

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Electrical Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF


Magnetos/Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Wheels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHOCKED

Wing/Tail tie downs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

AMD 11



Page 102


AMD 11


Page 103L CESSNA 172S (SP)Operating checklist and emergency procedures as per Flight Operations Manual forCessna model 172S (SP) Document Cessna 172SPHUS05.

BASIC AEROPLANE OPERATING CHECKLISTPRE FLIGHTAuthorisation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETEMaintenance Release . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSPECTED AND SIGNEDPre flight inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS PER HANDBOOKBaggage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE AND LOCKEDMandatory Documents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ABOARDTrip Sheet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOG START TIMEStart Position . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SUITABLE

STARTING ENGINE (With battery)1, Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN 1/4 INCH2, Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT OFF3, Propeller Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR4, Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON5, Flashing Beacon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Note; If engine warm, omit priming procedure of steps 6,7 and 8 below.6, Auxiliary Fuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON7, Mixture Set . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICH

(Until stable fuel flow is indicated, usually 3 to 5 seconds)Then set to idle cut off (Full Aft) position

8, Auxiliary Fuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF9, Ignition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START

(Release when engine starts)10, Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE

(Smoothly to rich when engine starts)Note: If engine floods (engine has been primed too much) turn off auxiliary fuel

pump, place mixture to idle cutoff, open throttle ½ to full and motor (crank)engine. When engine starts set mixture to full rich and close throttlepromptly.

11, Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK12, Navigation Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON as required13, Avionics Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON14, Radios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON15, Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT

AMD 11



Page 104

L CESSNA 172S (SP)

STARTING ENGINE (With external power)

1, Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN 1/4 INCH

2, Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT OFF

3, Propeller Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

4, Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

5, External power . . . . . . . . . . . . . . . . . . . . . . . CONNECT (to aeroplane receptacle)

6, Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

7, Flashing Beacon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Note: If engine warm, omit priming procedure of steps 8,9 and 10 below.

8, Auxiliary Fuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

9, Mixture Set . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICH

(Until stable fuel flow is indicated, usually 3 to 5 seconds)

Then set to idle cut off (Full Aft) position

10, Auxiliary Fuel Pump Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

11, Ignition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START

(Release when engine starts)

12, Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE

(Smoothly to rich when engine starts)

Note: If engine floods (engine has been primed too much) turn off auxiliary fuel

pump, place mixture to idle cutoff, open throttle/2 to full and motor (crank)

engine. When engine starts set mixture to full rich and close throttle

promptly.

13, Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

14, External Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISCONNECT

(From aeroplane receptacle, secure external power door)

15, Electrical System . . . . . . . . . . . . . . . . . . . . .CHECK FOR PROPER OPERATION

a) Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

(Disconnects both battery and alternator from the system)

b) Taxi and landing light switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

(to provide an initial electrical load on the system)

c) Engine RPM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE TO IDLE

d) Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

(with taxi and landing lights switched on)

e) Engine RPM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INCREASE TO 1500 RPM

(as engine RPM increases, alternator output should increase to meet the

system load requirements)

AMD 11



Page 105

L CESSNA 172S (SP)

STARTING ENGINE (With external power) (Cont’d)

f) Ammeter and low voltage annunciator . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

(the ammeter should indicate in the positive direction, showing that the

alternator is supplying current and the low voltage annunciator (VOLTS)

should not be lighted).

Note: If the indications as noted in steps “d” and “f” are not observed, the electrical

system is not functioning properly. Corrective maintenance must be

performed to provide for proper electrical system operation before flight.

16, Navigation Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON AS REQUIRED

17, Avionics Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

18, Radios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

19, Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT

AMD 11



Page 106

L CESSNA 172S (SP)

BEFORE TAKEOFF

1, Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

2, Passenger Seat Backs . . . . . . . . . . . . . . . . . . . . . . . . . . . . UPRIGHT POSITION

3, Seats and Seat Belts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK SECURE

4, Cabin Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED AND LOCKED

5, Flight Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FREE AND CORRECT

6, Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK AND SET

7, Fuel Quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

8, Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

9, Fuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RE CHECK BOTH

10, Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1800RPM

a) Magnetos.... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

(RPM drop should not exceed 150 RPM on either magneto or 50 RPM

differential between magnetos)

b) Vacuum gauge... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

c) Engine instruments and ammeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

11, Annunciator . . . . . . . . . . . . ENSURE NO ANNUNCIATORS ARE ILLUMINATED

12, Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK IDLE

13, Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM OR LESS

14, Throttle Friction Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST

15, Strobe Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

16, Radio and Avionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

17, NAV/GPS Switch (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

18, Autopilot (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

19, Manual Electric Trim (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

20, Elevator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET (For Take Off )

21, Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET (For Take Off 0 - 10E)

22, Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE

LINE UP

1, Compass / Directional Gyro . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ALIGN

2, Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ALT

AMD 11



Page 107

L CESSNA 172S (SP)

TAKE-OFF

NORMAL TAKEOFF

1, Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0 - 10º

2, Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPEN

3, Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

(Above 3000 feet LEAN to obtain maximum RPM)

4, Elevator Control . . . . . . . . . . . . . . . . . . . . . . . . LIFT NOSE WHEEL (at 55KIAS)

5, Climb Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 – 80 KIAS

6, Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT

SHORT FIELD TAKEOFF

1, Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10º

2, Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY


4, Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH


5, Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE

6, Elevator Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SLIGHTLY TAIL LOW

7, Climb Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 56 KIAS

(Until obstacles are cleared)


(Slowly after reaching 60 KIAS

AMD 11



Page 108

L CESSNA 172S (SP)

ENROUTE CLIMB

1, Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 — 85KIAS

2, Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL OPEN

3, Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH


CRUISE

1, Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2100 - 2700 RPM

(No more than 75% is recommended)

2, Elevator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST

3, Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN

DESCENT

1, Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

2, Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST FOR SMOOTH OPERATION

(Full rich for idle power)

3, Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

4, NAV/GPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

5, Fuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTH

6, Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

(0 - 10E below 110 KIAS, 10 - 30E below 85 KIAS)

BEFORE LANDING

1, Pilot and Passenger Seat Backs . . . . . . . . . . . . . . . . MOST UPRIGHT POSITION

2, Seats and Seat Belts . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURED AND LOCKED

3, Fuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTH

4, Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

5, Landing / Taxi Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

6, Autopilot (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

AMD 11



Page 109

L CESSNA 172S (SP)

LANDING

NORMAL LANDING

1, Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65 - 75 KIAS

(Flaps up)

2, Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED

(0 - 10º below 110 KIAS, 10 - 30º below 85 KIAS)

3, Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 60 - 70 KIAS

(Flaps down)

4, Touchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRST

5, Landing Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . LOWER NOSE WHEEL GENTLY

6, Braking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MINIMUM REQUIRED

SHORTFIELD LANDING

1, Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 65 - 75 KIAS

(Flaps up)

2, Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL DOWN (30º)

3, Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 61 KIAS

(Until flare)

4, Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE

(To idle after clearing obstacle)

5, Touchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRST

6, Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY HEAVILY


BALKED LANDING


2, Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT TO 20E3, Climb Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 60 KIAS

4, Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10E(Until obstacles are cleared)

RETRACT

(After reaching a safe altitude And 65 KIAS)

AMD 11



Page 110

L CESSNA 172S (SP)

AFTER LANDING


2, Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDBY

SECURING AEROPLANE

1, Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK LEFT AND RIGHT

2, Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

3, Electrical Equipment, Autopilot (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

4, Avionics Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

5, Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUTOFF

(Pulled full out)

6, Ignition Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

7, Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

8, Control Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSTALL

9, Fuel Selector Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEFT OR RIGHT

(To prevent cross feeding)

AMD 13


Page 111L PIPER PA31-350 CHIEFTAIN

Pre flight inspections and emergency procedures as per Piper Chieftain PA31-350Manufactures Information Manual.


PRE FLIGHT


PRE START

Baggage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURECabin Door & Safety Chain . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURESeats/Seat Backs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . POSITION & LOCKSeat Belts & Shoulder Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FASTENParking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SETFuel Valves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INBOARD TANKS – ONCrossfeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFFirewall Shutoff Valves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAlternate Air Valves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFCircuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK INElectrical Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAlternate Circuit Breaker Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONAvionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAlternate Static Source . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMALMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFuel Quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK 4 TANKSTrims . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET FOR TAKEOFFCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENGear Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GREENBaggage & Main Door Ajar Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFSeat Belts & No Smoking Signs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON (If Installed)Pilots Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LATCHEDTheft Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UNLOCKED (If installed)Fuel Boost Pump Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF (Press to Test)Fuel Flow Warning Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF (Press to Test)

AMD 13



Page 112

L PIPER PA31-350 CHIEFTAIN

STARTING

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT OFF

Emergency Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED (See POH)

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN ½ INCH

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL RICH FOR 5 secs then IDLE CUT OFF

Emergency Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED (See POH)

Prop Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPM

Magneto Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Props . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR

Starter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGE

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE AS ENGINE FIRES

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETARD AS REQUIRED TO 1000 RPM

Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Repeat last four (4) steps with other engine.

For Flooded Starts, Hot Starts and using APU, consult the POH

POST START

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .CHECK

Flashing Beacon and Navigation Lights . . . . . . . . . . . . . . . . . . . . . . . . . . ON as required

Ammeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Radios & Aids . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

TAXI

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . WORKING

Gyro Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Fuel Valves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK ALL POSITIONS

AMD 13



Page 113


PRE TAKE OFF


Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FORWARD

Prop Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FORWARD

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN


Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK & SET

Fuel Crossfeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1500 RPM

Alternator Output . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Vacuum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK (Min 4.3)

Prop Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FEATHER (Min 1000 RPM)

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2300 RPM

Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Prop Controls . . . . . . . . . . . . . . . . . . . . EXERCISE (Check Governor – 3x for 1st flight)

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CHECK

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

Flight Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL & FREE MOVEMENT

Harnesses & Hatches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE

Seat belt sign . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Crossfeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Fuel valves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INBOARD TANKS

Air conditioner . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF (if installed)

Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

Prop controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL FORWARD

Engine Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMAL

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0EAutopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Trims . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET FOR TAKE OFF

Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL AND FREE MOVEMENT

De-icing boots . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF (if installed)

Pre-Take Off Safety Brief . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE

AMD 13



Page 114


LINE UP

Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Strobes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

DG/Compass . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Pitot Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON AS REQUIRED

NORMAL TAKE OFF

Fuel flow warning lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL FORWARD

Manifold Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 43” CHECKED

Prop speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2575 RPM

Rotate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 88kts

Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Accelerate to . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 98kts

NORMAL CLIMB

Climb power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Cowl flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED

Emergency fuel pumps . . . . . . . . . . . . . . . . . . OFF (1 AT A TIME) CHECK PRESSURE

Air conditioner . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON AS REQUIRED (if installed)

Seat belt sign . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF AS REQUIRED

CRUISE

Fuel selectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

Cruise power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAN

DESCENT

Ensure EGT minimum 1350

Fuel valves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INBOARD TANKS

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET AS REQUIRED

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENRICHEN AS REQUIRED

AMD 13



Page 115


BEFORE LANDING

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TEST & OFF


Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICH

Fuel Selectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Seats, Belts & Harnesses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST & LOCK

Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

APPROACH

Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HIGH RPM

Undercarriage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK DOWN & LOCKED

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN

NORMAL LANDING

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PER P CHARTS

Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST

Touchdown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAIN WHEELS FIRST

Landing Roll . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOWER NOSE WHEEL GENTLY

Braking . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MINIMUM REQUIRED

AFTER LANDING

Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Pitot Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Strobe Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

AMD 13



Page 116


SHUTDOWN

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 RPM

Electrical & Radio Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK

Mixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE CUT-OFF

Ignition Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF after engines stop


Control Lock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INSTALL

ALL EMERGENCY PROCEDURES AND PERFORMANCE TAKE OFF AND LANDING

As per Pilot’s Operating Manual.

‘

AMD 14



Page 117

L PA-32R-301T, SARATOGA H TC

This Checklist is taken from Report VB-1647 issued June 30, 1997 up to and includingRevision dated March 11, 2002.

4.5 NORMAL PROCEDURES CHECKLIST

PREFLIGHT CHECK

COCKPITCAUTION: When draining any amount of fuel, care should be taken to ensure thatno rue hazard exists before starting engine.

Fuel Strainer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Drain & check for water & sedimentControl Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Release restraintsGear Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DownParking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SetAvionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAll switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Idle cut-offMagneto switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFBattery master switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFuel Gauges . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check quantityAnnunciator Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ExtendBattery Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFPrimary Flight Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Proper operationTrim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NeutralPitot And Static Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DrainWindows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check cleanRequired Papers and POH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check on boardTow Bar and Baggage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Stow properly - secureBaggage Door - Rear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Close and secure

AMD 14


Page 118

L PA-32R-301T, SARATOGA II TC

RIGHT WINGSurface Condition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Clear of ice, frost, snowFlap and Hinges . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckAileron and Hinges . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckStatic Wicks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check - secureWing Tip and Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckFuel Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check supply

visually - secure capFuel Quantity Gauge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckFuel Tank Vent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Clear

CAUTION: When draining any amount of fuel, care should be taken to ensure thatno fire hazard exists before starting engine

Fuel Tank Sump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Drainand check for water, sediment and proper fuel

Tie Down and Chock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RemoveMain Gear Strut . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Proper inflation

(4.00 ± .25 in.)Tire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckBrake Block and Disc . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckFresh Air Inlet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Clear

NOSE SECTIONGeneral Condition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckWindshield . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CleanBaggage Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Close and secureCowling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SecurePropeller and spinner . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckAir inlets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ClearEngine baffle seals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckChock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RemoveNose gear strut . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . proper inflation

(3.25 ± .25 in.)Nose Gear Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckNose wheel tire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckLanding Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SecureOil . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check quantityDipstick . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Properly seatedOil filler cap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Secure

AMD 14


Page 119


LEFT WINGSurface condition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Clear of ice, frost, snowFresh air inlet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Clear

CAUTION: When draining any amount of fuel, care should be taken to ensure thatno fuel hazard exists before starting engine.

Fuel Tank Sump. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Drain and check forwater, sediment and proper fuel

Tie Down and Chock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RemoveMain Gear Strut . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Proper inflation

(4.00 ± 25 in.)Tire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckBrake Block and Disc . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckFuel Tank Vent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ClearFuel Quantity Gauge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckFuel Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check supply

visually - Secure capStall Warning Vanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckPitot Head . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Remove cover - holes ClearWing Tip and Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckAileron And Hinges . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckFlap And Hinges . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckStatic wicks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check Secure

FUSELAGEAntennas . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckStatic Vents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ClearOxygen Discharge Disc . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check for ruptureEmpennage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Clear of ice, frost, snowStabilator and Trim Tab . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckTie down . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Remove

MISCELLANEOUSBattery Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . retractInterior Lighting. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON and CheckPitot Heat Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONPitot Heat OFF/INOP annunciator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

CAUTION: Care should be taken when an operational Check of the heated pitothead is being performed. The unit becomes very hot. Ground operation should belimited to three minutes to avoid damaging the heater elements.

AMD 14


Page 120


MISCELLANEOUS (CONT'D)

Exterior Lighting Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON and CheckPitot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check - warmStall Warning Horn . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckAll Lighting Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFPitot Heat Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFPitot Heat OFF/INOP Annunciator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONBattery Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFPassengers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BoardDoors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Closed and SecureSeats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Adjusted & LockedSeat Belts And Harness . . . . . . . . . . . . . . . . . . . . . . . . . fasten/adjust - Check inertia reel

NOTE: With the shoulder harness fastened and adjusted, a pull test of it's lockingrestraint feature should be performed.

ENGINE START - GENERALCAUTION: Do not attempt flight if there is no indication of alternator output.

CAUTION: If a positive oil pressure is not indicated within 30 seconds following anengine start, stop the engine and determine the trouble. In cold weather it will take afew seconds longer to get a positive oil pressure indication.

NOTE: Starter manufacturers recommend that starter cranking periods be limited to 30seconds with a two minute rest period between cranking periods. Longer cranking periodswill shorten the life of the starter.

BEFORE STARTING ENGINEBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SetCircuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check inAlternate Air . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full INCREASE rpmAvionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFFuel Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Desired tank

NORMAL START - COLD ENGINEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ½ in. openBattery Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONAlternator Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMagneto Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Prime - then idle cut-offPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ClearStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EngageMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full RICHThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AdjustOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

AMD 14


Page 121


NORMAL START - HOT ENGINEThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1/2 in. openBattery Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONAlternator Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMagneto Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Idle cut-offPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ClearStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EngageMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AdvanceThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AdjustOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

ENGINE START WHEN FLOODEDThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Open fullBattery Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONAlternator Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMagneto Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Idle cut-offPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ClearStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EngageMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AdvanceThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RetardOil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

STARTING WITH EXTERNAL POWER SOURCECAUTION: It is possible to use the ship's battery in parallel by turning only thebattery master switch ON. This will give longer cranking capabilities, but will notincrease the amperage. Care should be exercised because if the ship's battery hasbeen depleted, the external power supply can be reduced to the level of the ship'sbattery. This can be tested by turning on the battery master switch momentarilywhile the starter is engaged. If cranking speed increases, the ship's battery is at ahigher level than the external power supply.

NOTE: For all normal operations using external power, the battery master and alternatorswitches should be OFF.

Battery master switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAlternator switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFElectric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMagneto switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

AMD 14



Page 122


STARTING WITH EXTERNAL POWER SOURCE (CONT'D)

All Electrical Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

External Power Plug . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Insert in fuselage

Proceed with normal start

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Lowest possible RPM

External Power Plug . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Disconnect from fuselage

Battery Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Alternator switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON - Check ammeter

Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

WARM-UP

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 to 1200 RPM

TAXIING

Taxi Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Clear

Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Release

Prop . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . High RPM

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Apply slowly

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

Steering . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

NOTE: During taxi in hot and/or high altitude conditions, activation of electric fuel

pump may be required for smooth engine operation.

GROUND CHECK

Parking brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full INCREASE

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2000 RPM

Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Max. drop 175 RPM

- max. cliff. 50 RPM

Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Exercise - then

full INCREASE

AMD 14



Page 123


CAUTION: Alternate air is unfiltered, use of alternate air during ground or flight

operations when dust or other contaminant's are present may result in damage from

particle ingestion.

Alternate Air . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

Oil Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

Vacuum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check - within normal operating range

Annunciator Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Press-to-test

Air Conditioner . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

Ammeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

Electric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Fuel Flow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Retard

BEFORE TAKEOFF

Battery Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Verify ON

Alternator Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Verify ON

Electric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Magneto Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Verify ON

Engine Gauges . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full forward

Alternate air... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Fuel Selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Proper tank

Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Air conditioner . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Free

Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Latched

Seats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Adjusted & Locked

Seat Backs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Erect

NOTE: With the shoulder harness fastened and adjusted, a pull test of its locking

restraint feature should be performed.

Belts/Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fastened/Check

Empty Seats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Seat belts, Securely fastened

AMD 14



Page 124


TAKEOFF

NORMAL TECHNIQUE

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Retracted

Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . set

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set to maximum

Liftoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80 KIAS

Obstacle Clearance Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 85 KIAS

Landing gear (when straight ahead landing on runway not possible) . . . . . . . . . . . . . UP

SHORT FIELD, OBSTACLE CLEARANCE

NOTE: Gear warning will sound when the landing gear is retracted with the flaps

extended more than 10E.

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25ETrim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Apply

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set to maximum

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Release

Liftoff . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 70 KIAS

Obstacle Clearance Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75 KIAS

Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Up

Accelerate to climb speed

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Retract slowly

CLIMB

Best rate (3600 lb) (gear down)

(flaps up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 81 KIAS

Best rate (3600 lb) (gear up)

(flaps up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 95 KIAS

En route . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 105 KIAS

Electric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON


AMD 14



Page 125


CRUISE

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set per power table

Electric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Adjust


Fuel Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Proper tank

Seats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Adjusted & locked

Seat Backs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Erect

Belts/Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fasten/adjust

Electric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON


Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full increase

Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Down - 132 KIAS max.

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set - 110 knots max.

Air conditioner . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

NORMAL TECHNIQUE

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required

Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 90 KIAS

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required

SHORT FIELD TECHNIQUE

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40ETrim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80 KIAS

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required

GO-AROUND

Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full INCREASE

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full FORWARD

Control wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Back pressure to

rotate to climb attitude

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 80 KIAS

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Retract slowly

Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ss required

‘

AMD 14



Page 126


AMD 14



Page 127

L PA-44-180T, TURBO SEMINOLE

This Checklist is taken from Report VB-1100 issued March 14, 1980 up to and including

Revision dated October 10, 2005.

4.5 NORMAL PROCEDURES CHECK LIST

PREPARATION

Aeroplane Status . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Airworthy, papers on board

Weather . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Suitable

Baggage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Weighed, stowed, tied

Weight and C.G . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Within limits

Navigation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Planned

Charts and Navigation Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On board

Performance and Range . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Computed and safe

PREFLIGHT CHECK

INSIDE CABIN

Landing Gear Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN position

Avionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Landing Gear Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 GREEN

AMD 14



Page 128L PA-44-180T, TURBO SEMINOLE

Fuel Quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Adequate plus reserveCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMagneto switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFMixture Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Idle cut-offTrim Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NeutralFlaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check operationControls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FreePitot and Static Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DrainEmpty Seats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fasten beltsEmergency Exit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Closed and locked

OUTSIDE CABIN

Fuel Sump Drains . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Drain Right Wing, Aileron And Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check, no iceRight Main Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . No leaksStrut . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Proper inflationTire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckRight wing tip . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckRight leading edge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check, no iceFuel Cap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Open, Check quantity and

color, secureRight Engine Nacelle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check oilRight Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckCowl flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN and secureFuel drains . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DrainNose Section . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckNose gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . No leaksStrut . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Proper inflationTire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckTow bar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Removed and stowedLanding Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckWindshield . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CleanLeft Wing, Engine Nacelle and Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . Check as

on right sideStall warning vanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckPitot/static mast . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Clear, CheckedDorsal fin air scoop . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ClearEmpennage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check, no iceStabilator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FreeAntennas . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckNavigation and Landing Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckBaggage door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Secure and locked

AMD 14


Page 129


BEFORE STARTING ENGINESSeats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AdjustedSeat belts and Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fasten/adjust

Check inertia reelParking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

WARNINGNo braking will occur if aircraft brakes are applied whileparking brake knob is pulled and held.

Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . InRadios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFCowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPENCarburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFFAlternators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONProp Sync. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MANUAL

STARTING ENGINES

Fuel Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RICHThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1/4 inch openPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FORWARDMaster Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMagneto Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONPropeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ClearStarter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EngagePrimer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As req. - 2 seconds Max.Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Adjust when engine startsOil pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckRepeat for opposite engine.Alternators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckGyro suction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

NOTESWhen starting at ambient temperatures +20EF and below, operatefirst engine started with alternator ON (at max. charging rate notto exceed 1500 RPM) for 15 minutes minimum before initialisingstart on second engine.

If the STARTER ON light remains illuminated after the starterswitch is released, turn off the battery switch and shut down theengines.

AMD 14



L Page 130

PA-44-180T, TURBO SEMINOLE

STARTING ENGINES IN COLD WEATHER (BELOW 10EF)

If available, preheat should be considered. Rotate each propeller through 10 blades

manually during preflight inspection.

CAUTION

Insure magneto and master switches are OFF and mixture

controls are in idle cut-off before turning propeller manually.


External Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . connected

(See Starting Engines With External Power)

Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Electric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . full RICH

Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . full forward

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ¼ inch open

Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Starter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engage

Primer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON - 2 seconds Max.

Oil pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

If engine does not start, add prime and repeat above. When engine fires, prime as

required until engine is running smoothly.

External Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Disconnected

Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

STARTING ENGINES WHEN HOT

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ½ inch open

Master switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Electric fuel pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full RICH

Starter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engage

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Adjust

Oil pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

AMD 14



Page 131


STARTING ENGINES WHEN FLOODED

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Idle cut-off

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Open full

Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full forward

Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Magneto Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Electric Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Starter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engage

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Retard

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Advance


STARTING ENGINES WITH EXTERNAL POWER

Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

All Electric Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Terminals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Connect

External Power Plug . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Insert in fuselage

Proceed with normal start.

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Lowest possible RPM

WARNING

Shutdown the right engine when it is warmed prior to

disconnecting the external power plug.

External Power Plug . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Disconnect from fuselage

Master Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON - Check ammeter


Right Engine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Restart

WARM-UP

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1000 to 1200 RPM

AMD 14


Page 132


TAXIINGChocks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RemovedTaxi Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ClearThrottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Apply slowlyBrakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckSteering . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckInstruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckHeater and Defroster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckFuel Selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON, Check crossfeed

BEFORE TAKEOFF - GROUND CheckParking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONMixture Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FORWARDProp Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FORWARDProp Sync. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MANUALThrottle Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1500 RPMProp Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check feathering,

500 RPM max. dropThrottle Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2000 RPMProp Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check governor Prop Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full FORWARDCarburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckMagnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check, max. drop

175 RPM, max. diff.drop 50 RPM

Alternator Output . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CheckGyro Suction Gauge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4.8 to 5.2 in. Hg.Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 800-1000 RPMFuel selectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONElectric fuel pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONAlternators . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ONEngine Gauges . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . In the greenAnnunciator Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Press-to-testAltimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SetAttitude Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SetD.G. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SetClock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Wound and setMixtures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SetPrimers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check - OFFPropellers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set in forward position

AMD 14



Page 133


Quadrant Friction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Adjusted

Carburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Seat Backs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Erect

Seat Belts and Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fastened/adjusted

Empty Seats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Seat belts fastened

Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Free, full travel

Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Latched

Air Conditioner . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Pitot Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required

TAKEOFF

CAUTION

Fast taxi turns immediately prior to takeoff run should be avoided.

Adjust mixture prior to takeoff from high elevations. Do not over heat. Adjust mixture only

enough to obtain smooth engine operation.

NORMAL TAKEOFF (Flaps up)

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Accelerate to 75 KIAS.

Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Ease back to rotate

to climb attitude

After breaking ground, accelerate to best rate of climb speed of 88 KIAS.

Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

SHORT FIELD TAKEOFF (Flaps up)

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Stabilator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Takeoff range

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Takeoff power before brake release.

Accelerate to 70 KIAS.

Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Rotate firmly to attain

75 KIAS through 50 ft.

AMD 14



Page 134


Accelerate to best angle of climb speed of 82 KIAS for obstacle clearance or best rate of

climb speed of 88 KIAS, no obstacle.

Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

SHORT FIELD TAKEOFF (25E Flaps)

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25E (second notch)

Stabilator Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set

Takeoff power before brake release.

Accelerate to 63 K1AS.

Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Rotate firmly to attain

67 KIAS through 50 ft.

Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

TAKEOFF CLIMB

Best rate (flaps up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 88 KIAS

Best angle (flaps up) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 82 KIAS

En route . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 105 KIAS

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required

Electric Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

CRUISE CLIMB

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full RICH

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75%

Climb speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 105 KIAS

Cowl flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required


CRUISING

Reference performance charts and Avco-Lycoming Operator's Manual.

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set per power table

Electric Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF(ON if required

above 10,000 ft.)

Mixture Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Adjust

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required

AMD 14



Page 135


DESCENT

Propellers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2400 RPM

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required for 165 KIAS &

500 FPM descent

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 165 KIAS

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required

Carburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON if required

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Closed

Landing Gear & Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

DESCENT (Power off)

Prop. Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FORWARD

Throttles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Closed

Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . as required

Carburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Verify - throttle open &

closed every 30 seconds

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSED

Landing Gear & Wing Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP


Gear Warning Horn . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check

Seat Backs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Erect

Seat Belts and Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fasten/adjust

Fuel Selectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required


Mixture Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Rich

Prop sync. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MANUAL

Prop Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full FORWARD

Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN, 140 KIAS max.

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set, white arc

Approach Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 75 KIAS or above

Air Conditioner . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

AMD 14



Page 136


GO-AROUND

Full takeoff power, both engines.

Establish positive climb.

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Retract

Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Adjust

AFTER LANDING

Clear of runway.

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Retract

Cowl Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fully OPEN

Carburettor Heat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Electric Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

SHUTDOWN

Electric Fuel Pumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Radios . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full aft

Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Idle cut-off

Magnetos . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF


PARKING

Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required

Control Wheel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Secured with belts

Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Full up

Wheel Chocks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . In place

Tie Downs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Secure

‘




L Page 1

ACTION TO BE TAKEN IN THE EVENT OF AN ACCIDENT OR INCIDENT

INITIAL RESPONSE

Following an accident or incident involving a Club aircraft, Club staff attending the scene shall;

(1) Contact emergency services on 000;

(2) Use whatever means possible to suppress/extinguish any fire;

(3) Rescue injured personnel;

(4) Place injured in the recovery position and administer first aid;

(5) Secure the area to allow free access of emergency services.

NOTIFICATION

(1) Club staff shall immediately contact the Chief Pilot, the CFI or delegate who shall;

(a) notify ATSB by phone immediately; (1800 011 034)(b) notify the Club’s Insurance Company immediately.

(2) Information to be provided in initial report by the Chief Pilot or delegate

(a) Aircraft Type;

(b) Aircraft Registration;

(c) Location of accident site;

(d) Brief details of the damage, if know;

(e) Details of any injuries sustained.

SAFEGUARDING AIRCRAFT

(1) If the aircraft must be moved to clear an active runway, do so but ensure that photographs ofthe aircraft in "situ" are taken.

(2) If the aircraft is not presenting a hazard or at risk of further damage do not commencedismantling or removal until approval has been given.

(4) Take all possible steps to safeguard the wreckage. Where possible, take a photo of the panelbefore removing all documentation for safe keeping.

(5) Although in the initial stages the aircraft will, in all probability, be under the control of theAustralian Transport Safety Bureau, it is essential to maintain a "watching brief' in the absenceof the surveyor to ensure the security of the aircraft following its release.

(3) The pilot of the aircraft involved shall enter accident/incident on Maintenance Release.



L Page 2


COLLECTION OF ESSENTIAL DATA

The Chief Pilot or delegate shall arrange the collection and securing of the following data;

(1) Copy of Current Maintenance Release;

(2) Copy of Certificate of Registration;

(3) Copy of Certificate of Airworthiness;

(4) Computer printout or copy of aircraft maintenance and component status;

(5) Carry out survey of the damage and provide precise and detailed report;

(6) Organise an estimate of repair costs and proposed methods of repair.

REPORTING

(1) As soon as possible and at least within 24 hours, the pilot is to provide a fully detailed reportregarding the accident to the Chief Pilot, including events of the day and general informationregarding previous activities leading up to the accident.

(2) This report should include also;

(a) Weather details;

(b) Details of terrain at the accident site and surrounding areas;

(c) Weight and balance details;

(d) Licence details:

(I) Licence Category;

(ii) Licence Number;

(iii) Date of Issue;

(iv) Date of last renewal/flight review;

(v) Period of validity;

(vi) Details of ratings held;

(vii) Total flying experience on helicopters and/or aeroplanes;

(viii) Total flying experience on type involved in accident;

(ix) Total hours experience in the type of specialised operation involved.

(e) Your name;

(f) Your date of birth;

(g) Your address;

(h) The names of persons on board, if any;

(I) Details of any injuries received by them, if any.

(3) Details of any injuries sustained by the pilot as a result of the accident.



L Page 3


IN THE EVENT OF BODILY INJURY OR DEATH

(1) Do not admit liability or make or offer to make any payment to anyone.

(2) Actions by the pilot in command;

(a) Immediately contact Chief Pilot or Manager who will contact the Club’s insuranceprovider;

(b) Provide brief pertinent details plus the names(s) of a contact person able to becontacted, an after hours telephone number, a direct business telephone number andthe named location of the accident site;

(c) Shortly thereafter the insurance surveyor and/or appointed liability adjustor will contactyou and provide all further assistance.

(3) In the meantime appoint one person, preferably the principal of the business, to deal withpolice, ATSB and Insurance Surveyor.

(4) Appoint another mature person (one only) to handle:

(a) Telephone Calls (Log the date, time, number, name of person and message) theperson calling should be informed that;

"A person in a position to answer their enquiry will telephone them assoon as they are able to do so"

(b) Liaison for persons in (3) above;

(c) Administration tasks, ie. photocopying;

(d) Obtaining and preparing document file etc,

MEDIA (Press/TV) - A RECOMMENDED RELEASE IS AS FOLLOWS

“The aircraft accident is the subject of a full investigation by the authorities and it is notappropriate for us to comment or speculate on what may have happened pending theoutcome of this investigation. All enquires in relation in the accident should be directedto the Australian Transport Safety Bureau and all enquires in relation to persons onboard should be directed to (town) Police"

If deaths have resulted from the accident, include in the above statement;

“We wish to extend our sympathy and condolence to the relatives of the deceasedperson(s)”.

GG



Page 1

PRECAUTIONS WHEN USING HIGH PRESSURE OXYGEN

A.6.1.. The servicing of aircraft oxygen systems is to be carried out only by anappropriately rated LAME or a person who has Maintenance Approval for thepurpose.

A.6.2.. Oxygen by itself is a non-flammable oxidising gas, however oxygen vigorouslysupports combustion. Almost all materials are combustible and will burn moreactively and at higher temperatures in the presence of pure oxygen. Somematerials which do not burn in air will burn readily in oxygen enrichedatmospheres, some other materials may spontaneously combust in an oxygenrich environment, and if the concentration of oxygen is sufficiently high, thecombustion of these materials may take the form of a violent explosion.

A.6.3.. Contamination In Oxygen Systems

(1) Contaminants in oxygen systems are potential fire or explosion hazards.When a gas is compressed it releases energy in the form of heat. When thegas is compressed quickly inside a closed system such as a container orpiping, temperatures inside the system can rise sharply. In an oxygen system,this rise in temperature can be high enough to cause explosive ignition ofcontaminants such as oil, grease, solvents and materials such as dust, lint,metal chips and many organic materials.

(2) Oxygen flowing at high speed through valves and piping systems can alsopropel contaminants with such force that friction or impact between particlescan raise their temperature to the ignition point. The ignition of these particlesmay be enough to cause heavier metal sections to ignite and cause a majoraccident.

A.6.4.. Moisture In Oxygen Systems

(1) The presence of moisture in an oxygen system with valves located in anunheated parts of the aircraft may cause the valves to freeze, rendering thesystem inoperative. Moisture may also cause internal cylinder corrosion,sufficient cause for condemning the cylinder.

(2) In order to help prevent moisture contamination, aircraft oxygen systemsshould only be charged with Aviators Breathing Oxygen.

....


08/07 THE REDCLIFFE AERO CLUB Section A6L FLIGHT CONDUCT Appendix 4

Page 2

PRECAUTIONS WHEN USING HIGH PRESSURE OXYGEN

A.6.5.. Minimum Positive Pressure

A cylinder that has been fully depleted may allow the ingress of moisture and/orcontaminants so oxygen cylinders should be maintained at a positive pressure atall times. Cylinders that have been depleted to zero PSI must be removed from theaircraft and internally inspected prior to refilling.

A.6.6.. Safety Precautions

(1) The following safety precautions should always be followed:

(a) Always handle bottles and gauges with care.

(b) Do not drop pressurised components;

(c) Allow only authorised, approved personnel to service, repair or overhauloxygen equipment;

(d) Follow the manufacturer's instructions for operation, maintenance andoverhaul procedures;

(e) Never use oil or grease in, on or around oxygen equipment;

(f) Ensure that tools used are clean of contaminants and are non-sparking;

(g) Do not improvise or substitute parts or materials on oxygen systems;

(h) Do not expose oxygen systems to high temperatures, and keep awayfrom all combustibles;

(i) Do not smoke in an aircraft when an oxygen system is being refuelled orin use;

(j) Ensure that only "Aviators Breathing Oxygen" is used when refilling anoxygen system;

(k) Ensure the aeroplane and the refilling equipment are earthed to theground and the refilling equipment connected to the aeroplane by theuse of static lines before hoses are connected to the refilling connectionof the oxygen system to prevent electrostatic discharge;

(l) Ensure oxygen valves are opened slowly;

(m) Always do a preflight check of your oxygen system in accordance withthe checklist in the Pilot's Operating Handbook for the particularaeroplane or the Operator Manual for portable systems.




SECTION A7

SAFETY MANAGEMENT AND AUDITING

INDEX

SUB-SECTION PAGE

SAFETY POLICY STATEMENT A7-2

7.1 GENERAL A7-3

7.2 OBJECTIVES A7-3

7.3 SAFETY MANAGEMENT PERSONNEL A7-4

7.4 REPORTING AND INVESTIGATION A7-5

7.5 HAZARD IDENTIFICATION AND RISK MANAGEMENT A7-6

7.6 DOCUMENT CONTROL A7-7

7.7 INTERNAL AUDITS A7-8

7.8 FUEL QUALITY AUDIT PROGRAM A7-9

APPENDIXES

1. RISK SEVERITY, LIKELIHOOD AND RISK RATING MATRIX TABLES

2. CONFIDENTIAL SAFETY REPORT FORM

3. HAZARD IDENTIFICATION AND RISK ASSESSMENT REPORT

4. FUEL COMPANY AUDIT REPORT



04/04 SAFETY MANAGEMENT AND AUDITING A7-2


SAFETY POLICY STATEMENT

This statement sets out to guide Club staff on health, safety, environmental andconservation matters and security in the work environment.

The Club's objectives are:

· To provide a safe and healthy working environment.

· To secure personal safety at work.

· To prevent hazards to the health of their own employees, contractors, customersand other third parties.

· To promote the reporting of all hazards, incidents, accidents, lost time injuriesand first aid uses through the Club and regulatory reporting systems. The Clubapproach will be non-punitive (where possible), investigating all reports to gainthe maximum learning from these reports.

· To promote environmental conservation.

· To enhance the security of all persons in the Club premises, and protect theClub assets.

· To protect the Club reputation, by demonstrated HSE standards and results.

These objectives have a high priority and equal status with the primary businessobjectives. Everyone working within the Club premises or on Club aircraft shouldparticipate, since achieving these objectives requires their active commitment.




7.1 GENERAL

(1) The safe and effective operation of Club aircraft is the primary goal of the Club.Each and every Club employee must maintain an active interest to achieve thisgoal.

(2) The Club shall utilise an internal program to collect and identify any information,experiences or occurrences which may present a hazard to Club operations.

7.2 OBJECTIVES

(1) The primary objective is the achievement and maintenance of a high standardof safety in Club operations by;

(a) Identification of inadequate information, practices and procedures andsafety hazards;

(b) Receipt and management of Confidential Hazard Reports and safetyinformation records;

(c) Conducting of confidential surveys of Club staff;

(d) Conducting audits on all aspects of Club operations and administration;

(e) Review and address any non-conformance affecting Club operations; and

(f) Conduct safety meetings with Club staff when required for the gatheringand dissemination of safety issues.

(2) No person will be penalised for submitting a Confidential Hazard Report.





7.3 SAFETY MANAGEMENT PERSONNEL

(1) The Club shall appoint the following persons to the Safety Committee;

(a) The President;

(b) the Chief Pilot; and

(c) the Safety Officer.

(2) The duties of the Safety Committee shall include;

(a) to oversee the conduct of the Safety Management System;

(b) conducting meetings on the request of the Safety Officer;

(c) formulating responses to the recommendations of the Safety Officer;

(d) formulating and implementing changes to the Safety Committee;

(e) formulating reports to the responsible external organisation where anaction required to prevent an identified hazard is outside the control of theClub.

(3) Chief Executive Officer of the Club shall implement the safety managementsystem and encourage its use in Club operations on a continuing basis. Theduties of the Chief Executive Officer shall include;

(a) conducting management reviews of the effectiveness of the safetymanagement system and recommend changes to the Safety Officer;

(b) requesting the Safety Officer to convene meetings of the Chief Pilot andSafety Officer to discuss management initiatives;

(c) implement recommendations from the Safety Officer in relation tomanagement practices.

(4) Chief Pilot of the Club shall encourage the continued use of the safetymanagement system by Club personnel under his/her control. The duties of theChief Pilot shall include;

(a) conducting operational reviews the effectiveness of the safetymanagement system and recommend changes to the Safety Officer;

(b) requesting the Safety Officer to convene meetings of the Safety Committeewhen required to discuss operational initiatives;

(c) implement operational recommendations from the Safety Officer.....




7.3 SAFETY MANAGEMENT PERSONNEL

(5) Safety Officer of the Club shall be responsible for the implementation of theClub's Safety Management System. His/her duties shall include;

(a) the maintenance, review and revision of the Club's Safety ManagementSystem;

(b) conducting internal audits of Club procedures or organising an auditconducted by an external organisation;;

(c) maintaining the Club's Confidential Safety Reporting System and thereceipt, review, evaluating and monitoring of the Confidential HazardReports submitted by Club personnel as detailed in sub-section 7.4(2);

(d) formulating recommendations on Confidential Hazard Reports as detailedin sub-section 7.5 for consideration by the Safety Committee;

(e) convening the Safety Committee to discuss the effectiveness of thesystem, and implementation of recommendations on safety matters raisedby Club employees;

(f) evaluate the effectiveness of emergency procedures training andrecommend changes in the Club's training or operations;

(g) conduct safety meetings of pilots and other Club personnel associated withthe conduct of flight operations;

(h) reminding Club personnel of their duties and responsibilities regardingground and flight safety;

(i) source and distribute safety articles, videos, posters and other safetymaterial relevant to Club operations; and

(j) where appropriate, the submission of information to external organisations.

7.4 REPORTING AND INVESTIGATION

(1) If an incident/event occurs during the normal performance of duties that wasconsidered potentially unsafe, a Confidential Hazard Report shall be completedand sent/handed to Safety Officer for subsequent investigation. It is a systemby which all Club staff can report any concerns they may have about safetywithin the Club.




7.4 REPORTING AND INVESTIGATION

(2) On receipt of a Confidential Hazard Report the Safety Officer shall;

(a) de-identify the report;

(b) segregated the report into four areas; (i) Flight Operations;(ii) Engineering;(iii) Ground Handling; and(iv) Security.

(c) the Safety Officer shall then conduct hazard identification and riskmanagement as detailed in sub-section 7.5.

(d) the Safety Officer shall report back to the person who submitted theReport.

(3) All Confidential Hazard Reports will remain active and responses torecommended action shall be monitored by the Safety Officer.

7.5 HAZARD IDENTIFICATION AND RISK MANAGEMENT

(1) Upon receipt of a Confidential Hazard Report, the Safety Officer shall;

(a) determine if any reports identifying similar hazards have been submitted;(b) evaluate the seriousness of the hazard; (c) evaluate the level of risk;(d) evaluate the likelihood of the hazard recurring;(e) evaluate the adequacy of established Club practices and controls;(f) determine the action and Club resources required to eliminate or control

the hazard and prevent similar occurrences;(g) determine under whose area of responsibility the action required falls and

recommend the action required.

(h) if the hazard is outside the control of the Club, place the findings beforethe Safety Committee for the formulation of a report to the responsibleexternal organisation.

(2) The Safety Officer shall use the tables in Appendix 1 to this Section as a guideto determining the risk rating of a defined hazard.

(3) The Safety Officer shall complete a Hazard Identification and AssessmentRecord to provide a record of identified hazards and the actions taken by theresponsible person to address the risks.




7.5 HAZARD IDENTIFICATION AND RISK MANAGEMENT

(4) All actions shall be assigned to the specific person responsible for that area ofClub operations. A target date for implementation of the action must be given.

(5) The Hazard Identification and Assessment Record shall not be closed until therequired action is implemented. The record shall be retained in order to providereference for review of results and future risk assessments.

7.6 DOCUMENT CONTROL

(1) the following documentation is used in the safety management system;

(a) Confidential Hazard Report - Appendix 2

(b) Hazard Identification and Assessment Record - Appendix 3

(2) Upon receipt of a Confidential Hazard Report, the Safety Officer shall assign anidentification number in the form of YYMM##.

(3) This number shall be used to identify all documentation concerned with thatparticular Report.

(4) Where an amendment is made to a document during the safety managementprocess, an amendment number is to be added to the identification number thus;YYMM## / #.

(5) All Confidential Hazard Reports and associated documents shall be filed underthe following headings;(a) Flight Operations;(b) Engineering;(c) Ground Handling; and(d) Security.

(6) The Safety officer shall review all Confidential Hazard Reports and associateddocuments every 12 months. Records may be destroyed;

(a) 2 years after the actions to prevent the hazard have been implementedand no recurrence of the hazard has occurred; or

(b) after the aircraft type to which the hazard referred is no longer operated bythe Club; or

(c) after the type of operation to which the hazard referred is no longerconducted by the Club.




7.7 INTERNAL AUDITS

(1) The Safety Officer shall conduct audits of the Club operations;

(a) annually;

(b) following the introduction of a new aircraft type;

(c) following the change of any key personnel;

(d) following the change of a maintenance organisation.

(2) The areas of audit shall include;

(a) the completeness of Club documentation;

(b) management and supervision procedures;

(c) Club's accident and incident prevention approach;

(d) Club flight operating procedures;

(e) passenger handling procedures;

(f) operations around aircraft on the ground;

(g) aircraft refuelling;

(h) aircraft maintenance control;

(i) dissemination of safety related material;

(j) completeness in the training of Club staff;

(k) performance of the Club in relation to safety matters;

(l) staff participation in safety management;

(m) working environment.

(3) The person conducting the audit shall record any perceived deficiencies and

determine the risk rating for those deficiencies on a Confidential Hazard Report.

(4) All of these Reports shall be subject to the hazard identification and risk

management process detailed in sub-section 7.5 above.




7.8 FUEL QUALITY AUDIT PROGRAM

(1) The Club shall establish and maintain a fuel quality audit program for all fuel

used in Club operations in accordance with this sub-section.

(2) Before the initial purchase of fuel and every twelve months where that supplier

or agent continues to supply fuel for Club use, a fuel Club supplier or agent shall

be subject to an audit by the Chief Pilot. A copy of the Club Fuel Company Audit

Record is shown at Appendix 4 to this Section.

(3) The Club shall only purchase fuel from Mobil, Caltex, BP or Shell or their

accredited agents who have met the requirements of the Club's fuel quality audit

program.

(4) When drumstock fuel is received by the Club, it shall be checked to ensure the

drums are in good condition with no major damage, no leaking, original seals

intact and product details such as brand, filling date, grade and batch number

are clearly visible. If otherwise, the drum must be rejected and the matter

reported to the Chief Pilot.GG


04/04 THE REDCLIFFE AERO CLUB Section A7SAFETY MANAGEMENT AND AUDITING Appendix 1

Page 1RISK SEVERITY, LIKELIHOOD AND RISK RATING MATRIX TABLES

Hazard identification is the determination of a condition with the potential of causing injury to Clubpersonnel, damage to Club equipment or reduction in the ability to perform a function. Risk is the chanceof injury or loss and the magnitude.

SEVERITY

4 Catastrophic • Loss of aircraft.• Multiple fatalities.

3 Hazardous • Large reduction in safety margins.• Physical distress or a high workload such that flight crew. cannot be relied

upon to perform their tasks accurately or completely.• Serious or fatal injuries to a relative small number of occupants.

2 Major • significant reduction in safety margins.• Reduction in the ability of the flight crew to cope with adverse operating

conditions impairing their efficiency.

1 Minor • Nuisance.• operating limitations or emergency procedures.

LIKELIHOOD

4 Probable • May occur once or several times during operational life.

3 Remote • Unlikely to occur during total operational life of each system but may occurseveral times when considering several systems of the same type.

2 ExtremelyRemote

• Unlikely to occur when considering systems of the same type, butnevertheless, has to be considered as being possible.

1 ExtremelyImprobable

• Should virtually never occur in the whole fleet life.

Risk Rating Matrix

Severity ?

Catastrophic 44

Review8

Unacceptable12

Unacceptable16

Unacceptable

Hazardous 33

Acceptable6

Review9

Unacceptable12

Unacceptable

Major 22

Acceptable4

Review6

Review8

Unacceptable

Minor 11

Acceptable2

Acceptable3

Acceptable4

Review

Likelihood <Extremely

Improbable1

ExtremelyRemote

2Remote

3Probable

4

To determine the Risk Rating, enter the Risk Rating Matrix Table from the left in the row correspondingto the Severity rating and move right to the column corresponding to the Likelihood rating. The RiskRating is where the row and column intersect.



SAFETY MANAGEMENT AND AUDITING Appendix 2

Page 1


CONFIDENTIAL SAFETY REPORT FORM

This form is a confidential means of reporting any concerns you have about safety within the Club. If youfeel that, during the performance of your duties, you experienced or witnessed an event that was potentiallyunsafe, please complete the form below and send/hand it to the Club Safety Officer. By submitting a reportyou will help identify unsound practices or facilities that may comprise the flying school’s safety, or ultimately,the safety of Club employees. If you have any questions regarding this reporting system, please contact theSafety Officer

Location: Date: Time:

Fully describe the occurrence;

Recommendations for corrective action (if any):

In your opinion, what is the worst possible outcome if this occurrence occurred again? (Circle one)

Catastrophic Hazardous Major Minor

In your opinion, what is the likelihood of this occurrence happening again? (Circle one)

Probable Remote Extremely Remote Extremely Improbable

Identification Number: Assigned by the Safety Officer

E ----------------------------------------------------------------------------------------------------

Name: (Your name will be kept confidential)

Please provide your name so that we can clarify any information you have submitted. Once the Safety Officer have investigated the report, thistear off strip will be returned to you with a brief report on what remedial action has been taken to prevent recurrence of this event. No recordof your name will be kept. Use the identification number for all communications with the Safety Officer

Identification Number: Assigned by the Safety Officer


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Page 1




Page 1


FUEL COMPANY AUDIT REPORT

FUEL COMPANY: LOCATION:

COMPANY REPRESENTATIVE: DATE:

ITEM SATISFACTORY

View bridger receipt documentation Yes No

Check tank release sheet for last 12 months Yes No

Check daily checks records on fuel farm tanks Yes No

Check daily checks records on refuelling equipment Yes No

Carry out visual inspection of facility for tidiness, organisation and potentialhazards

Yes No

Take sample of fuel and test for contaminates and density Yes No

All drums are stored so as to prevent contamination Yes No

Fuel quality checks are carried out on bulk fuel before filling drums Yes No

Empty drums are checked for damage before filling Yes No

Drums are fitted with metal capseals upon filling Yes No

Drums are handled in a way to prevent damage Yes No

Records are kept of batch number and filling date of drumstock. Yes No

REMARKS:

CHIEF PILOT: DATE:




SECTION A8

DANGEROUS GOODS ADMINISTRATION

SUB-SECTION PAGE

8.1 GENERAL A8-3

8.2 DANGEROUS GOODS TRAINING A8-3

8.3 TYPES OF DANGEROUS GOODS CARRIED A8-4

8.4 ACCEPTANCE PROCEDURES A8-4

8.5 STOWAGE A8-6

8.6 LOADING A8-6

8.7 INSPECTION FOR DAMAGED OR LEAKING PACKAGES A8-7

8.8 DAMAGED PACKAGES PROCEDURES A8-8

L 8.9 CONFISCATED OR UN-DECLARED DANGEROUS GOODS A8-10

L 8.10 ACTION IN THE EVENT OF A FIRE ON THE GROUND A8-11

L 8.11 DANGEROUS GOODS INCIDENTS IN FLIGHT A8-12




SECTION A8

DANGEROUS GOODS ADMINISTRATION

APPENDIXES

1. COPY OF SUB-SECTION 2.3 and TABLE 2.3.A OF THE IATA DANGEROUS

GOODS REGULATIONS

2. DANGEROUS GOODS IN OPERATOR’S PROPERTY

3. HIDDEN DANGEROUS GOODS

4. UNDECLARED DANGEROUS GOODS OCCURRENCE REPORT

5. PACKING INSTRUCTION 650

L 6. Reserved

L 7. Reserved

L 8. Reserved

L 9. NOTIFICATION TO PILOT OF DANGEROUS GOODS IN CREW OR

PASSENGER BAGGAGE



03/06 DANGEROUS GOODS ADMINISTRATION A8-3

8.1 GENERAL

(1) This Section forms the Club’s Dangerous Goods Manual. Only the dangerousgoods listed in sub-section 8.3 are approved to be carried on board Clubaircraft.

L (2) Only dangerous goods listed in sub-section 8.3(1)(a) may be carried on Clubaeroplanes whilst passengers are on board.

8.2 DANGEROUS GOODS TRAINING

(1) Club employees shall be classified into “Groups” to define their duties andresponsibilities and the level of training required. A person may, depending onhis/her duties, require training under one or more Groups.

(2) Club employees shall be classified for the purpose of dangerous goodstraining in accordance with the following;

DUTIESEMPLOYEE GROUP

Group A Group B Group C Group E

All Flight Crew X X

Ground baggage and cargo handlers X

(3) Club employees shall complete training in relation to dangerous goods inaccordance with the following;

Group A; A CASA approved Group A training course designed to enable a person toaccept cargo which contain dangerous goods.

Group B: A CASA approved Group B training course designed to enable a person toaccept cargo not containing dangerous goods.

Group C: A CASA approved Group C training course. A person who has completed thislevel of training shall not accept passenger or crew baggage nor cargo forcarriage on board Club aircraft.

Group E: A Group E training course designed to enable a person to handle cargo andpassenger checked or carry-on baggage. A person who has completed thislevel of training shall not accept cargo for carriage on board Club aircraft.

(4) Subject to CASR 92.090, this training shall be successfully completed everytwo years.

(5) The person conducting the courses Group A thru C must have approval underCASR 92.140. The person conducting a Group E training course shall havesatisfactorily completed a Group A or B training course within the previous 2years.




8.3 TYPES OF DANGEROUS GOODS CARRIED

(1) The following dangerous goods may be accepted for carriage on board a Clubaircraft:

(a) Those stated on sub-section 2.3 and Table 2.3.A of the IATA DangerousGoods Regulations. Refer to Appendix 1 to this Section;

(b) Articles and substances detailed in sub-section 2.5 of the IATADangerous Goods Regulations “Dangerous Goods in Operator’sProperty”. Refer to Appendix 2 to this Section;

(c) Diagnostic specimens provided that the contents are packed inaccordance with the requirements of IATA Packing Instruction 650.Refer to Appendix 5 to this Section.

8.4 ACCEPTANCE PROCEDURES

(1) Passenger and Crew Baggage

(a) Before a person offers baggage for carriage on board an aircraft in whichhe/she is travelling, the person conducting the acceptance of baggageshall inform the owner of the following;

(i) the restrictions on the carriage of dangerous goods;

(ii) information on dangerous goods that are permitted in baggage orcarriage by the person and which of those goods that requireapproval of the Club in accordance with Section 2.3 of the IATADangerous Goods Regulations (Appendix 1 to this Section).

(b) The owner of the baggage shall be asked to declare any acceptabledangerous goods and to remove any other dangerous goods. Refer tosub-section 8.4(2) for processing dangerous goods in crew andpassenger baggage;

(c) If the passenger declares that there are no dangerous goods, baggagecan be accepted for carriage on board Company aeroplanes. TheCompany retains the right to ask the passenger to open the baggage forinspection.

(2) Dangerous Goods in Crew and Passenger Baggage

(a) The person accepting the baggage shall determine if the declareddangerous goods are permitted for carriage in accordance with Appendix1 to this Section; ....





(2) Dangerous Goods in Crew and Passenger Baggage (Cont’d)

(b) Where permitted dangerous goods require approval of the Company forcarriage, the check in staff shall;

(i) inform the owner of the baggage that approval is required; and

(ii) give that approval where the quantity and packaging meets therequirements of Appendix 1;

(iii) enter an approval number in the Passenger and Cargo Manifestrelating to passenger name, time, date and the name of thep e r s o n w h o h a s g i v e n t h e a p p r o v a l ,(passengerhhmmDDMMYYname) eg. Smith1458290805bloggs forSmith 14:58 29/08/05 Bloggs.

(c) Baggage containing permitted dangerous goods that may only be carriedin checked baggage shall be accepted from the passenger and loadedon board the aircraft in a locker not accessible by the passenger;

(d) Where the pilot in command must be informed of the location of thedangerous goods, complete a “Notification to Pilot of PermittedDangerous Goods in Crew and Passenger Baggage” and hand it to thepilot in command. A copy of this Notification is shown at Appendix 9 tothis Section.

L (e) Each item of checked baggage containing dry ice must be marked withthe Dry Ice Baggage Tag shown on Page 4 of Appendix 1.

(f) Dangerous goods not permitted shall be removed from the baggagebefore the baggage is accepted for carriage. It is the responsibility of thepassenger for the safe removal of these dangerous goods fromCompany premises.

(3) Cargo Not Containing Dangerous Goods

(a) The Club shall make available to intended shippers of cargo a ClubConsignment Note.

(b) The Club requires that a person who consigns any cargo for carriage onboard a Club aircraft to describe the contents and make a writtenstatement that the cargo does not contain dangerous goods bycompleting and signing a Club Consignment Note. This shall becompleted in triplicate. A copy of the Consignment Note is shown atAppendix 3 to Section A4; ....





(3) Cargo Not Containing Dangerous Goods

(c) If any doubt exists regarding a particular consignment, the consignormust be asked to check the description of the cargo against the generalclass listings of dangerous goods in the ICAO Technical Instructions forthe Safe Transport of Dangerous Goods by Air or the IATA DangerousGoods Regulations and confirm that no part of the consignmentcontains dangerous goods, otherwise that shipment cannot be carriedon board a Club aircraft;

(d) The person accepting the cargo on behalf of the Club shall check thatthe Consignment Note has been completed correctly and shall inspectthe cargo to for indications of hidden dangerous goods. Examples ofhidden dangerous goods is shown in Appendix 3 to this Section;

(e) Passengers shall be asked to declare that their baggage does notcontain any dangerous goods;

(f) The acceptance of this cargo shall only be conducted by a person whohas completed Group A or Group B training.

(4) On any occasion when undeclared dangerous goods are discovered in cargoor when dangerous goods not permitted under the provisions of this Sectionare discovered in passengers baggage, an Undeclared Dangerous GoodsOccurrence Report outlining the incident shall be forwarded to CASA withintwo working days. A copy of the Club Undeclared Dangerous GoodsOccurrence Report is shown at Appendix 4 to this Section.

8.5 STOWAGE

(1) Packages containing dangerous goods which may react with each other must bestored in positions that would not allow interaction in the event of leakage.

(2) The following table shows the separation of incompatible dangerous goodsthat are permitted to be carried on board Club aircraft.

Class or Division 1.4S 2 3 8

1.4S - - - -

2 - - - -

3 - - - -

8 - - - -

(3) An "X" at the intersection of a row and a column indicates that packagescontaining that Class or Division of dangerous goods must be physicallyseparated.




8.6 LOADING

(1) The pilot in command shall be satisfied of correct identification of anydangerous goods to be carried, the nature, the UN number(s) and loadedposition by means of loading the substance(s) personally or personallysupervising the loading of the substance(s) prior to flight.

(2) All dangerous goods loaded in an aircraft must be protected from damage andsecured in a manner that will prevent any movement in flight which wouldchange the orientation of the packages.

(3) Packages containing liquid dangerous goods must be loaded and stowedaboard an aircraft in accordance with the package orientation "this wayup"/"this end up" label. Single packagings with end closures containing liquiddangerous goods must be loaded and stowed aboard the aircraft with thoseclosures upwards, notwithstanding that such single packages may also haveside closures.

(4) All dangerous goods being loaded or unloaded shall be inspected for damageas detailed in sub-section 8.7, below.

8.7 INSPECTION FOR DAMAGED OR LEAKING PACKAGES

(1) Before and after carriage on Club aircraft, all dangerous goods shall beinspected for damage or leakage by a Club pilot.

(2) If evidence of damage or leakage is found the procedures detailed in 8.9below shall be carried out.

(2) If any package is found to be damaged or leaking, it shall be isolated and thatpackage stored apart from all other goods until safe disposal can be arranged.If the package is leaking and the resultant leakage is liable to cause injury ordamage, the following shall be notified immediately;

(a) local fire services;

(b) Club management;

(c) airport authorities; and

(d) the shipper.

(3) If any damage or leakage from packages is found by other Club staff, theChief Pilot shall be notified immediately.

(3) The areas of the aircraft where dangerous goods have been stowed or carriedshall be visually inspected for contamination immediately following removal ofsuch substances. Any contamination found shall be removed before any othergoods are placed in those areas.




8.8 DAMAGED PACKAGES PROCEDURES

(1) In the event of damage occurring to a package containing dangerous goods,the following procedures, as applicable to the class of dangerous goods shallbe carried out.

(2) Explosives - (Class 1.4S)

(a) If a package bearing the 'EXPLOSIVE' label has been damaged, ensurethat there is no risk of a naked flame or spark and that the contents arenot subjected to friction.

(b) Should a fire or explosion occur, try to prevent the fire from spreadingbut if unsuccessful:

(i) Evacuate the immediate vicinity

(ii) Call police, fire and other emergency services, as appropriate

(iii) Administer first aid as required.

(3) Gases - Compressed Or Liquid (Class 2)

(a) Flammable, compressed or liquefied gas is liable to give off vapourwhich may cause suffocation, or be ignited by a spark or flame.

(b) There is also the risk of explosion if the cylinders are subjected to undueheat.

(c) Should a leak from a faulty or damaged valve occur, move the defectivecylinder into the open and thoroughly ventilate the place where it hadbeen stowed to remove any trace of escaped gas. Remember somegases are heavier than air and any escaped gas will thereforeconcentrate at the lowest level of the storage area.

(4) Flammable Liquids (Class 3). Refer also to sub-section 5.17 of Section A5.

(a) vapour is leaking, ensure the package is exposed to maximumventilation and minimum temperature, and safeguard against possibleignition by spark or flame; or

(b) liquid is leaking, prevent it from spreading by soaking up with anabsorbent material. Do not attempt to wash it away as the use of watermay spread the danger further; or

(c) If fire occurs, move containers that are exposed to flames/heat if thiscan be done without risk, apply appropriate fire extinguisher/s to seat offlames and call local emergency services. ....


© AEROSERVICE 2000


8.8 DAMAGED PACKAGES PROCEDURES

(5) Oxidising Substances (Class 5.1)

(a) Oxidisers are strong supporters of combustion and will readily stimulate

fires. Oxygen is a strong supporter of combustion and can cause self

ignition of finely divided organic material.

(b) vapour is leaking, ensure the package is exposed to maximum

ventilation and minimum temperature, and safeguard against possible

ignition by spark or flame; or

(c) liquid is leaking, prevent it from spreading by soaking up with an

absorbent material. Do not attempt to wash it away as the use of water

may spread the danger further; or

(d) If fire occurs, move containers that are exposed to flames/heat if this

can be done without risk, apply appropriate fire extinguisher/s to seat of

flames and call local emergency services.

(6) Corrosives (Class 8)

(a) Corrosives are any liquid or solid material which is considered to be

destructive to materials and metals or which may cause irreversible

alteration to human skin and other living tissue. Fumes can be

dangerous if inhaled and can also cause severe irritation to the eyes.

(b) If a package bearing the 'CORROSIVE' label is found to be leaking, provide

maximum ventilation, avoid skin contact and inhalation and protect eyes.

(c) There is also the risk of fire where a corrosive substance comes into

contact with an organic material or other chemicals, as chemical action

can generate considerable heat leading to spontaneous combustion.

(d) Isolate the hazard if this can be done without risk, but do not attempt to

cleanse the area where the leak had occurred except under supervision.

If the leak occurs in an aircraft an appropriately licensed aircraft

maintenance engineer shall conduct the supervision.




L 8.9 CONFISCATED OR UN-DECLARED DANGEROUS GOODS

(1) The Company shall hold confiscated or un-declared dangerous goods in a

secure area isolated from all other goods. These goods shall be surrendered

to the CASA upon request.

(2) When confiscated or un-declared dangerous goods are not required by the

CASA, the Company shall contact the owner and request arrangements be

made for their collection.

(3) Where these dangerous goods are not collected or the owner cannot be

contacted, the Company shall quarantine and store the dangerous goods in

a secure area isolated from all other goods.

(4) If these dangerous goods are not collected after a period of 3 months, the

Company shall;

(a) take ownership of the goods;

(b) contact the manufacturer of the dangerous goods and obtain the correct

disposal method;

(c) dispose of the goods in the method acceptable to the type of dangerous

goods.





L 8.10 ACTION IN THE EVENT OF A FIRE ON THE GROUND

(1) Following an alert to a fire in Company premises, Company staff shall

(a) Contact emergency services on 000;

(b) Switch off any electrical services to the affected area;

(c) Rescue any injured personnel, place injured in the recovery position and

administer first aid;

(d) Secure the area to allow free access of emergency services.

(2) After the initial actions have been completed, the following is to be used as an

initial course of action in an attempt to contain the fire pending the arrival of

local emergency services;

(a) Move people from the area, upwind for preference;

(b) Extinguish cigarettes and naked lights;

(c) Apply available extinguishers, the order of preference being Dry Powder,

CO2 or Water.

CAUTION

If the materials involved are combustible liquids or solids, flammable

liquids, liquid oxidisers, corrosive liquids and the like, the use of water

may spread or intensify the fire.

(d) Avoid contact with burning material and avoid breathing smoke or fire

generated vapours or gas; wear breathing apparatus and protective

clothing if available;

(e) Remove other cargo from the immediate area to prevent spread of fire;

(f) Attempt to stop any spillage from spreading, or from entering

underground drains, by banking with sand or earth;

(3) If the fire gets out of control before the arrival of the police or fire brigade,

evacuate the area and warn against entry.




L 8.11 DANGEROUS GOODS INCIDENTS IN FLIGHT

(1) If an in-flight emergency occurs and the situation permits, the pilot in commandmust inform the appropriate Air Traffic Services Unit of any dangerous goodson board the aircraft. This information should include the proper shippingname and/or UN number, the class/division and in the case of explosives, thecompatibility group, any identified subsidiary risk(s) and the quantity andlocation on board the aircraft. If it is not possible to include all the information,those parts thought most relevant should be given.

(2) In Flight

(a) Follow the appropriate emergency procedures in the helicopter check listfor fire or smoke control;

(b) Consider landing at nearest landing point, especially if operating withoutany other person on board;

(c) Consider turning off non-essential electrical equipment;

(d) Determine source of fire/smoke/fumes;

(e) Advise passengers and seek their help if needed;

(f) If it is absolutely certain that the item will not create a problem thedecision may be made not to move it. If is necessary to move the item,this should be done as suggested below;

(i) using rags, paper etc, place the item in a polyethylene bag, emptyesky or other plastic container;

(ii) place the container in a position as far away as possible from thecockpit and/or passengers;

(g) If time permits, notify ATS of at least the UN number of the dangerousgoods on board.

(3) After Landing

(a) Disembark any passengers before opening any cargo compartmentdoors.

(b) Inform ground personnel/emergency services of nature of the dangerousgoods involved and where stowed.

(c) Make appropriate entries in the Maintenance Release.

‘


01/09 THE REDCLIFFE AERO CLUB Section A8L DANGEROUS GOODS ADMINISTRATION Appendix 1

Page 1



Page 2



Page 3



Page 4



Page 5



Page 6



Page 1

DANGEROUS GOODS IN OPERATOR'S PROPERTY

2.5 Dangerous Goods in Operator's Property

STATE VARIATION: CHG-01

2.5.1 Exemptions

The provisions contained in these Regulations do not apply to the articles and substances of 2.5.1.1 through 2.5.1.3.

2.5.1.1 Aircraft Equipment

Articles and substances which would otherwise be classified as dangerous goods but which are required to beaboard the aircraft in accordance with pertinent airworthiness requirements and operating regulations or that areauthorised by the State of the operator to meet special requirements.

2.5.1.2 Consumer Goods

Aerosols, alcoholic beverages, perfumes, colognes, safety matches and liquefied gas lighters carried aboard apassenger aircraft by the operator for use or sale on the aircraft during the flight, or series of flights, but excludingnon-refillable gas lighters and those lighters liable to leak when exposed to reduced pressure.

2.5.1.3 Carbon Dioxide, Solid (Dry Ice)

Carbon dioxide, solid (dry ice) for use in food and beverage service aboard the aircraft.

2.5.2 Aircraft Spares

2.5.2.1 Unless otherwise authorised by the State of the operator, articles and substances intended asreplacements for those referred to in 2.5.1.1 must be transported in accordance with the provisions of theseRegulations, except that when consigned by operators, they may be carried in containers specially designed fortheir transport, provided such containers are capable of meeting at least the requirement for the packaging specifiedin these Regulations for the items packed in the containers.

2.5.2.2 Unless otherwise authorised by the State of the operator, articles and substances intended asreplacements for those referred to in 2.5.1.2 and 2.5.1.3 must be transported in accordance with the provisions ofthese Regulations.



DANGEROUS GOODS ADMINISTRATION Appendix 3

L Page 1




L Page 2



L DANGEROUS GOODS ADMINISTRATION Appendix 4

Page 1


UNDECLARED DANGEROUS GOODS OCCURRENCE REPORT

Date: Airport: Aircraft:

Location: ~ Inflight ~ In Aircraft On Ground ~ Ground Handling

~ Baggage Area ~Other

BAGGAGE DETAILS

Passenger’s Name:

Passenger’s Address:

CARGO DETAILS:

Sender’s Name:

Sender’s Address:

Receiver’s Name:

Receiver’s Address:

Consignment Note completed: ~ Yes ~ No Number:

MARKING OF UNDECLARED DANGEROUS GOODS

Class Hazard Label affixed to goods: ~ Yes ~ No

Proper Shipping Name:

Class: UN Number on goods:

DETAILS OF OCCURRENCE

Description Of Occurrence

Prepared By: . . . . . . . . . . . . . . . . . . . . . . . . . Both . . . . . . . . . . . . . . . . . . . . . . Signature: Date:




L Page 1




L Page 2




L Page 1


NOTIFICATION TO PILOT OF PERMITTED DANGEROUSGOODS IN CREW OR PASSENGER BAGGAGE

Where the pilot in command must be informed of the location of the permitted dangerous goods, the personaccepting passenger baggage shall complete this form and hand it to the pilot in command.

Aircraft Reqd VH-

Departure: Destination:

Pax Name:

Description of Baggage:

Dangerous Goods:

Class/Division: Class 8 ‘Name/Description:

Mercury Barometer or Thermometer ‘

Spillable battery (Wheelchair or mobility aid) ‘Location in Aircraft:

Completed By: Date:

Pilot in Command: Date:


03/09 THE REDCLIFFE AERO CLUB A10-1

L DRUG AND ALCOHOL MANAGEMENT PLAN

SECTION A10

INDEX

TITLE PAGE

POLICY STATEMENT A10-2

10.1 DEFINITIONS A10-3

10.2 INTRODUCTION A10-9

10.3 APPLICATION A10-9

10.4 DUTIES AND RESPONSIBILITIES A10-10

10.5 DRUG AND ALCOHOL EDUCATION PROGRAM A10-13

10.6 DRUG AND ALCOHOL TESTING PROGRAM A10-14

10.7 DRUG AND ALCOHOL TESTING PROCESS A10-17

10.8 DRUG AND ALCOHOL RESPONSE PROGRAM A10-18

10.9 SELF-REFERRAL A10-22

10.10 ROLE OF THE MEDICAL REVIEW OFFICER A10-22

10.11 DISCIPLINARY ACTION A10-23

10.12 PRIVACY, REPORTING AND RECORDS A10-23

10.13 REVIEW, VARIATIONS, AUDIT AND COMPLIANCE A10-24

APPENDIXES

1. DAMP AWARENESS TRAINING RECORD

2. EMPLOYEE’S DAMP RECORD

3. REASONABLE SUSPICION RECORD

4. DRUG AND ALCOHOL RESPONSE RECORD

5. TRAINING RESOURCES



03/09 DRUG AND ALCOHOL MANAGEMENT PLAN A10-2

POLICY STATEMENT

The health, well-being and safety of personnel are of paramount importance

to the Club. All individuals have a right to be safe at the Club’s workplace.

Alcohol and Other Drugs (AOD), when present in persons in the workplace,

have the potential to increase risk of harm in the workplace and adversely

impact upon fitness for work.

The Club has a duty of care to minimise the risk of accident, incident and

injury in the workplace arising from the consumption of alcohol or other

drugs. The purpose of this policy is to outline the strategies and processes

that will be used by the Club to manage the risks associated with use, or

recent use, of alcohol or other drugs by persons in the workplace.

The Club takes a multi-strategy approach that incorporates education,

support, testing and performance management. The policy is based on

safety outcomes and not whether a positive test result is illicit or legal. This

policy also recognises permissible therapeutic drug use under the guidance

of a physician or pharmacist.




10.1 DEFINITIONS (to be read in conjunction with sub-section 0.2, Section AO, Part A)

Accident means an occurrence that arises out of a person performing or beingavailable to perform an applicable safety-sensitive aviation activities (SSAA) ifeither or both of the following applies:

(a) the occurrence results in the death of, or serious harm to, a person;

(b) the occurrence results in serious damage to an aircraft or property.

Aerodrome testing area means:

(a) any surface in a certified aerodrome or registered aerodrome over which anaircraft is able to be moved while in contact with the surface of theaerodrome, including any parking areas; and

(b) any part of the surface of a certified aerodrome or registered aerodrome:

(i) that is not covered by paragraph (a); and

(ii) that does not have a building on it; and

(iii) form which access to a surface mentioned in paragraph (a) may be had;and

(c) a building located on a certified aerodrome or registered aerodrome that isused:

(i) for maintenance of an aircraft or an aeronautical product; or

(ii) for the manufacture of aircraft or aeronautical products; or

(iii) by an air traffic service provider to control air traffic; or

(iv) by the holder of an AOC for flying training; and

(d) any part of an aircraft, aerobridge or other moveable structure in a certifiedaerodrome or a registered aerodrome.

....




10.1 DEFINITIONS

Appropriately qualified alcohol and other drug professional means a person

who:

(a) materially works as a provider of clinical drug and alcohol treatment services;

and

(b) holds a bachelor degree, or postgraduate degree, in at least 1 of the following

fields:

(i) health sciences;

(ii) medical science;

(iii) social sciences;

(iv) behavioural sciences.

Comprehensive assessment means an examination of the person’s physiological

and psychosocial indicators carried out:

(a) by a psychiatrist; or

(b) by a medical practitioner who is a Fellow of the Australasian Chapter of

Addiction Medicine; or

(c) jointly by:

(i) a person entitled to practise as a medical practitioner under a law of a

State or Territory; and

(ii) an appropriately qualified drug and alcohol professional.

Crew Member means any person having duties, other than as a flight crew

member, on board a Club aircraft who are essential to the successful conduct of

the operation being performed by that aircraft. For Club operations, a crew member

may be a camera operator during photography, a person assisting with the

navigation of the aircraft, a client required to define areas to be surveyed or

avoided or a person being trained for these duties.

DAMP contact is the person nominated to CASA by Club and charged with overall

responsibility for liaison with CASA about Club drug and alcohol testing

responsibilities.

....




10.1 DEFINITIONS

DAMP Medical Review Officer is a person who meets the following criteria:

(a) a registered medical practitioner

(b) has competence in the field of interpreting drug and alcohol test results

(c) has knowledge of substance use disorders

(d) has knowledge of the relevant provisions of the CASRs.

DAMP Supervisor means a person who has received appropriate training to order

to form an opinion as to whether a person may be adversely affected by a testable

drug or under the influence of alcohol. He/she has also received training on

aspects of prevention and management of problematic AOD use under the DAMP.

It is the DAMP Supervisor to whom employees report their concerns about

medications they are taking. Additionally, the DAMP Supervisor has access to the

DAMP Medical Review Officer (MRO) for advice and clarification as required.

Drug or Alcohol Intervention Program may consist of any of the following:

(a) assessment

(b) treatment, including:

(i) education

(ii) counselling

(iii) consultation with health care professionals

(iv) pharmacotherapy

(v) residential or non residential treatment programs

(c) monitoring and follow up action

Flight Crew Member means any person carrying out duties on a Club aircraft who

are essential to the flying or safety of the flight of that aircraft.

Management means the Club administration and includes any person who is

responsible for managing, directing or controlling Club affairs.

....




10.1 DEFINITIONS

Permitted level means:

(a) for alcohol, a concentration of less than 0.02 grams of alcohol in 210 litres of

breath

(b) for a testable drug, a concentration of the testable drug that is specified in a

legislative instrument made by CASA for the purposes of CASR 99.010.

The permitted level in urine for each testable drug;

Testable Drug Level - ug/L

Morphine 300

Codeine 300

6-Acetyl morphine 10

Amphetamine 300

Methylamphetamine 300

Methylenedioxymethylamphetamine 300

Δ9-tetrahydrocannabinol 10 15

Benzoylecgonine 150

Ecgonine methyl ester 150

The permitted levels in oral fluid for each testable drug;

Testable Drug Level - ng/mL

Morphine 25

Codeine 25


Amphetamine 25



Methylenedioxyamphetamine 25


Cocaine 25

Benzoylecgonine 25


Note: These levels ensure that the results are administratively reliable and are set

at a sufficient level to detect recent alcohol or drug use by the donor. ....




10.1 DEFINITIONS

Positive result means the following:

In relation to a drug or alcohol test of a body sample the test results reveals:

(a) for an initial drug test - a test result above the permitted level.

(b) for a confirmatory drug test - a test result above the permitted level andverified by a Medical Review Officer (MRO) as a verified positive result

(c) for an initial alcohol test - a test result above the permitted level

(d) for a confirmatory alcohol test - a test result above the permitted level

Regular SSAA employee means a SSAA employee who is reasonably likely toperform an applicable SSAA at least 2 or more times every 90 days.

Safety-sensitive aviation activities that are undertaken by the Club and/or Clubcontractors are:

(a) any actions taken by a person in an aerodrome testing area (including thepersons presence in the area) other than as a passenger;

(b) any of the following activities, wherever they occur;

(i) the weight and balance calculations of aircraft;

(ii) the maintenance, certification of maintenance or manufacture of aircraft,aeronautical products, ground based navigation aids or radar;

(iii) the fuelling and maintenance of vehicles that will be used to fuel aircrafton aerodrome testing areas;

(iv) activities undertaken by an airport security guard or screening person inthe course of their duties as a guard or person;

(v) activities undertaken by a member of the operating crew of an aircraft inthe course of that persons duties as a crew member;

(vi) the loading and unloading of baggage trolleys and the driving of tugs;

(vii) providing flight information and search and rescue alert services to apilot or operator of an aircraft immediately before or during the flight ofthe aircraft or as an intermediary for communications between a pilot oroperator of the aircraft and an air traffic controller.

....




10.1 DEFINITIONS

Serious incident is an occurrence that is associated with the manufacture,

maintenance or operation of an aircraft, aeronautical product or ground based

navigational aid if either or both of the following applies:

(a) the occurrence gives rise to danger of death or serious harm to a person; or

(b) the occurrence gives rise to danger of serious damage to an aircraft or

property.

Suspension Event means an event where this program requires a SSAA

employee to cease performing or being available to perform a SSAA

Testable drug group is any of the following:

Amphetamines

Cannabis

Cocaine

Opiates




10.2 INTRODUCTION

(1) This document is the The Redcliffe Aero Club Drug and Alcohol Management

Plan (DAMP). The Club is required by Part 99 of the Civil Aviation Safety

Regulations 1998 (CASRs) to develop and implement a DAMP, covering

persons who perform, or are available to perform, a safety-sensitive aviation

activity (SSAA).

(2) This Drug and Alcohol Management Plan (DAMP) has been developed to

meet the requirements of the CASR 99 from material distributed by CASA.

(3) In addition to meeting the statutory obligations of the Club, the aim of this

DAMP is to minimise the risk of alcohol and other drug use that may affect

the health and safety of Club employees, contractors, sub-contractors and

passengers.

(4) The Management of the Club will ensure that the consumption of drugs or

alcohol will not take place on Club premises or in an area where SSAA’s are

conducted.

10.3 APPLICATION

(1) This DAMP applies to all The Redcliffe Aero Club personnel who perform, or

are available to perform, a SSAA.

(2) These personnel are;

(a) persons employed directly by the Club;

(i) flight crew;

(ii) crew members;

(iii) ground crew.

(b) contractors engaged by the Club;

(c) subcontractors engaged by contractors of the Club; and

(d) persons employed by those contractors and subcontractors.

(3) In this program the personnel listed in (2) above are all referred to as “SSAA

employees” even though they may not be directly employed by the Club.




10.4 DUTIES AND RESPONSIBILITIES

(1) Club

(a) The Club is legally required to, and will, comply strictly with its

obligations under this program.

(b) The Club shall ensure training is provided and the DAMP made available

to existing Club employees and contractors currently performing SSAAs

before 23 March 2009;

(c) The Club shall ensure training is provided and the DAMP made available

to Club employees and contractors required to perform SSAAs after 23

March 2009;

(d) the Club shall not to permit an employee or contractor to perform

SSAAs;

(i) where the DAMP Supervisor suspects impairment due to the

person being under the influence of a testable drug or alcohol;

(ii) when a serious incident or accident has occurred involving the

employee or contractor while performing or able to perform

SSAAs;

- for the period that suitable test conditions exist for conducting

drug or alcohol tests on the employee - a test has not been

conducted; or

- if tests have been conducted - the Club has not been notified of

the test results.

(iii) if a SSAA employee has been required to cease performing, or

being available to perform, SSAA duty because of an incident related

to alcohol or drugs, not permit that SSAA employee to again

perform or be available to perform SSAA duty until all mandatory

pre-conditions detailed in 10.8 have been met.

(e) provide periodic reports to CASA about its administration of this DAMP

or its dealings with its SSAA employees who have been subject to

alcohol or drug testing by CASA.





(2) Contact Officer

(a) The Contact Officer shall;

(i) liaise with CASA including being informed, where required, of the

results CASA testing events.

(ii) maintain an up to date “Employee’s DAMP Record” for each Club

employee.

(3) DAMP Supervisors

(a) DAMP Supervisors shall receive training about how to form an opinion

as to whether a person may be adversely affected by a testable drug or

under the influence of alcohol and are authorised by the Club to form

such an opinion in appropriate cases.

(b) DAMP Supervisors shall undertake periodic training to develop and

maintain knowledge relevant to their role as DAMP Supervisor.

(c) Where a DAMP Supervisor forms that opinion, they must require a SSAA

employee or a SSAA contractor to cease performing or being available

to perform a SSAA. Where required to do so by a DAMP Supervisor, a

SSAA employee of the Club or a SSAA contractor must cease

performing or being available to perform a SSAA.

(d) DAMP Supervisors, in cases where the testing program has been

breached, shall ensure;

(i) appropriate utilisation of counselling and disciplinary procedures.

(ii) counselling of employees who have had positive test results or

who have referred themselves is available.

(iii) rehabilitation plans for Club employees, as advised by a suitable

qualified health professional, is agreed to.

(e) The DAMP Supervisor shall display information to inform visitors entering

an area on the Club premises where SSAA’s are conducted;

(i) that they may be subject to random drug and alcohol testing

conducted by CASA; and

(ii) their requirements to conform to the Club's DAMP.





(4) Club SSAA Employees and SSAA Contractors

(a) Management expects that all SSAA employees will comply with their

obligations under this DAMP. SSAA employees;

(i) must not perform, or be available to perform, a SSAA if aware that

they are adversely affected by a testable drug or by alcohol, until

they are no longer adversely affected;

(ii) are subject to drug and alcohol testing under this program while

performing, or being available to perform, a SSAA;

(iii) will be required to provide a body sample if they are to be tested

for drugs and alcohol by the Club for the purposes of conducting

such tests;

(iv) must cease performing or being available to perform SSAAs if they:

- return a positive result for a drug or alcohol test;

- fail to comply with a request by an approved tester to provide a

body sample for CASA drug and alcohol testing;

- fail to comply with a request to provide a body sample for the

Club drug and alcohol testing under this program;

- interfere with a body sample they provide for drug or alcohol

testing by CASA or the Club.

(v) if required to cease performing, or being available to perform,

SSAA duty because of an incident related to alcohol or drugs,

must not again perform or be available to perform SSAA duty until

all mandatory pre-conditions have been met.

(b) Club employees are encouraged to disclose to the DAMP Supervisor if

they have consumed a level of alcohol, or have taken any drug, that may

affect their ability to carry out a SSAA. Failure to do so may result in;

(i) them committing an offence against the CASRs; and/or

(ii) the Club taking disciplinary action against its employees or

contractual action against contractors or sub-contractors. ....




10.5 DRUG AND ALCOHOL EDUCATION PROGRAM

(1) All SSAA employees and DAMP Supervisors are required to complete a drug

and alcohol education program detailed in Appendix 5 to this Section.

(2) The Club will ensure that all SSAA employees and DAMP Supervisors have

access to an education program in accordance with the following;

(a) for SSAA employees and DAMP Supervisors employed by the Club prior

to 23 March 2009, before 23 March 2009; and

(b) for personnel who are to become SSAA employees and DAMP

Supervisors after 23 March 2009, at induction and prior to the employee

performing or being available to perform a SSAA.

(3) The Club will additionally provide refresher education to all SSAA employees

at an interval of no longer than 30 months.

(4) The Club drug and alcohol education program for SSAA employees covers

awareness of;

(a) Club policy on drug and alcohol use; and

(b) drug and alcohol testing in the workplace; and

(c) support and assistance services for people who engage in problematic

use of drugs and alcohol; and

(d) information about the potential risks to aviation safety from problematic

use of drugs and alcohol.

(5) In addition to the training in (4) above, DAMP Supervisors shall receive

education and training to manage people who engage in problematic use of

drugs or alcohol.

(6) On the completion of the Awareness Training, the employee shall complete

the Club's DAMP Awareness Training Record. The Record shall be

countersigned by the DAMP Supervisor. A copy of this record is shown at

Appendix 1 to this Section.




10.6 DRUG AND ALCOHOL TESTING PROGRAM

(1) The Club will test for the following substances;

Alcohol Cannabinoids Opiates

Ampehtamines Cocaine

(2) Drug and Alcohol Limits

Alcohol - Club employees and contractors must have less than 0.02 breath

alcohol content (BAC) when present in the aerodrome testing area or

performing safety sensitive aviation activities. Any breath alcohol test

registering equal to or greater than the prescribed limit above shall be

deemed a positive result.

Drugs - Individuals must return a negative drug test result for testable drugs

at all times while in the aerodrome testing area or performing safety sensitive

aviation activities on behalf of the Club. On-site initial drug testing will assess

the drug classes and concentrations in Table 1.

TESTABLE DRUG PERMITTED LEVELS IN URINE

TESTABLE DRUG LEVEL - ug/L

Morphine 300

Codeine 300


Amphetamine 300




Benzoylecgonine 150


(3) In addition to the drug and alcohol testing conducted by or on behalf of the

Club under this program, SSAA employees (including all persons who

perform duties in an aerodrome testing area) may also be subject to random

drug and alcohol testing by CASA under CASR Part 99.C.

(4) The Club does not perform random testing of Club employees. ....





(5) Drug and alcohol testing of all Club SSAA employees under this program will

only be conducted in the following circumstances;

(a) A person will be tested for alcohol and testable drugs when they first join

the Club, if the person will be working as a regular SSAA employee, or

when the role of an existing employee is to change to that of a regular

SSAA employee, unless the person has been drug and alcohol tested

less than 90 days before the person is required to begin performing or

being available to perform a SSAA and the test results were not positive

results.

(b) A person will be tested for alcohol and testable drugs after an accident

or serious incident involving a SSAA employee that occurs whilst they

are performing, or available to perform, a SSAA, provided that suitable

test conditions exist. Refer to 10.6(7) below.

(c) A Club SSAA employee will be tested if a DAMP Supervisor has

reasonable grounds to believe that employee may be adversely affected

by an alcohol or testable drugs while performing, or available to perform,

a SSAA. The DAMP Supervisor shall complete a “Reasonable Suspicion

Record” detailing the grounds, testing and results. A copy of this record

is shown at Appendix 3 to this Section.

(d) A Club SSAA employee will be tested for alcohol and testable drugs if

that employee is returning to work after a period during which the

employee was not permitted under the CASRs to perform or be available

to perform a SSAA because of alcohol or testable drug use or a related

incident.

(e) A Club SSAA employee who has returned a positive test result under

this program shall undergo subsequent testing for alcohol and testable

drugs in the one month period following the return to work in order to

monitor the employee’s ongoing compliance with this program.

(6) If a confirmatory drug test conducted under this program returns a positive

result, the Club will consult a DAMP Medical Review Officer to determine if

the presence and level of a testable drug detected by the test could be the

result of legitimate therapeutic treatment or some other innocuous source.....





(7) Suitable test conditions exist where, after an accident or serious incident,

testing can be conducted:

(a) within 32 hours of the accident or incident for drug testing;

(b) within 8 hours of the accident or incident for alcohol testing; and

(c) it is practicable to conduct a test.

(8) Club testing shall be conducted in accordance with the following matrix.

TESTING MATRIX ORAL FLUID URINE ALCOHOL

Pre-employment - X Breath

Post Incident/Accident - X Breath

Reasonable suspicion and confirmation - X Breath

Random and confirmation - X Breath

Before return to SSAAs - X Breath

Follow up testing - X Breath

(9) Any drug and alcohol testing carried out under this program will be performed

by accredited external technicians and conducted in accordance with the

following Australian Standards;

TESTING TYPE AUSTRALIAN STANDARDS

Alcohol AS 3547 – Breath alcohol testing devices for personal use.

NMI R 126 – Pattern Approval Specifications for Evidential

Breath Analysers

Drugs AS 4308 – Procedures for specimen collection and the detection

and quantitation for drugs of abuse in urine

AS 4760 – Procedures for specimen collection and the

detection and quantitation for drugs in oral fluid

(10) Any devices used in drug or alcohol testing under this DAMP must be used

in a way that is not inconsistent with the instructions of the manufacturer of

those devices.




10.7 DRUG AND ALCOHOL TESTING PROCESS

(1) Pre-employment drug or alcohol testing undertaken by a prospective

employee shall be conducted by a testing provider at the prospective

employee’s expense. The test for drugs shall be in the form of urine testing.

The results of this testing shall be presented to the Club DAMP Supervisor

before the employee engages in SSAAs.

(2) Club employees conducting non-SSAAs who are to engage in SSAAs at the

request of the Club, shall undergo drug or alcohol testing conducted by a

testing provider nominated by the Club at Club's expense.

(3) Where drug or alcohol testing is requested by the DAMP Supervisor, the

testing shall be conducted by a testing provider nominated by the Club. Where

circumstances permit, this test shall be carried out onsite. The method of

testing shall be in accordance with sub-section 10.6(8).

(4) Refusal to submit to, or co-operate fully with the administration of an alcohol

or other drug test will be treated as a positive result. Failure to provide a

sample to an authorised CASA tester is an offence under CASR Part 99 and

penalties apply.

(5) Adulteration of an individuals’ sample or tampering with the sample in any way

will be regarded as a breach of policy and treated as a positive screening.

(6) Where an individual returns a positive alcohol reading (a reading of 0.02

BAC), a confirmatory test will be conducted by the testing provider 15 minutes

after the initial test. If the second test confirms the initial reading, the

management processes set out in 10.8 will apply.

(7) Where an individual returns a initial positive drug test, they will be required

to provide a second sample for confirmatory screening at an accredited

laboratory.

(8) Confirmatory tests for alcohol will be conducted 15 minutes after the initial

test. Confirmatory testing for other drugs may take up to three days and is to

be conducted off-site by an accredited laboratory.

....




10.7 DRUG AND ALCOHOL TESTING PROCESS

(9) The testing procedure shall be witnessed at all times by both the donor and

the approved tester. The sample shall be split into sample A and sample B,

Splitting the sample ensures that the same sample that was tested in the

approved laboratory (sample A), is available in a second secure tamper proof

container (sample B) for the donor if they choose to get the sample tested

again. The donor can elect to have the B sample tested by the same

laboratory that tested sample A, or have it transported using strict chain of

custody procedures to a second approved laboratory.

10.8 DRUG AND ALCOHOL RESPONSE PROGRAM

(1) The DAMP Supervisor shall complete a “Drug and Alcohol Response Record”

detailing the testing and results. A copy of this record is shown at Appendix

4 to this Section.

(2) Where an employee’s initial drug test indicates a positive result for at least

one of the testable drugs and the confirmatory testing confirms a negative

test result or an “innocent positive”, i.e. legitimately required/prescribed

medication, or the DAMP Medical Review Officer determines the positive test

is the result of legitimate therapeutic treatment or some other innocuous

source, that employee will not be subjected to any disciplinary processes.

However that employee shall be counselled as to;

(a) the dangers of prescription and “over the counter” medication; and

(b) the need to inform the employee’s medical practitioner or chemist of the

type of employment undertaken by the employee.

(3) Where a Club employee returns a positive initial test for drugs conducted in

accordance with this program or as a result of CASA random testing, that

employee will not be permitted to perform SSAA. The employee shall be

stood down from duty and safe transport home will be provided.

(4) In the event a contractor returns a positive initial test, the contractor will not

be permitted to perform SSAA for the Club at that time. The contractor’s

employer shall be contacted and the employee will be required to provide

safe transport home for their employee.

....





(5) Any contractor found to be in violation of the Club's Drug and Alcohol Plan

will be refused entry into, or removed, and/or may be temporarily or

permanently suspended from visiting or providing services to the Club.

(6) The Club will not permit a SSAA employee to perform, or be available to

perform, a SSAA in any of the following circumstances;

(a) where the Club is aware that a positive result for an initial drug test has

been recorded and the employee has not, in respect of that test result,

recorded a test result for a confirmatory drug test that is not a positive

result.

(b) where the Club is aware that a positive result for an initial alcohol test

has been recorded and the employee has not, in respect of that test

result, recorded a test result for a confirmatory alcohol test that is not a

positive result.

(c) where the Club is aware under this DAMP or under CASA random

testing conducted in accordance with CASR Part 99;

(i) a positive result for a confirmatory drug test has been recorded for

the employee; and

(ii) a DAMP Medical Review Officer has not determined that the result

recorded could be because of legitimate therapeutic treatment or

some other innocuous source; and

(iii) mandatory preconditions for return to work have not been met.

(d) where the Club is aware that a SSAA employee who has been required

to take a drug or alcohol test has;

(i) refused to take the test; or

(ii) interfered with the integrity of the test.

(e) if a DAMP Supervisor suspects the employee’s faculties may be

impaired due to the person being under the influence of a testable drug

or alcohol;

....





(6) The Club will not permit a SSAA employee to perform a SSAA... (Cont’d)

(f) if an accident or serious incident has occurred involving the employee

whilst they are performing or available to perform a SSAA and either;

(i) for the period that suitable test conditions exist for conducting drug

or alcohol tests on the employee - a test has not been conducted;

or

(ii) if tests have been conducted under suitable test conditions - the

Club has not been notified of the test results.

(7) Following the first positive breath alcohol and/or drug screen, and subject to

involvement of a DAMP Medical Review Officer (MRO), the following

response actions will then be taken by the Club in relation to the employee;

(a) The DAMP Supervisor will discuss the drug and alcohol policy breach

with the employee.

(b) The employee will be removed from Club SSAAs and will not be

permitted to return to SSAAs until;

(i) the confirmatory test has confirmed a negative result; or

(ii) the employee has met all requirements of CASA Part 99 in regard to

returning to SSAA following a confirmed positive result.

(c) The employee will be issued with a written warning and will be required

to undergo a comprehensive assessment for drug or alcohol use and

participate in any nominated drug or alcohol intervention program.

(8) Where an employee returns a positive result after a suspension from SSAAs

due to a positive test result, that employee shall be dismissed.

(9) Where the Club has not permitted a SSAA employee to perform, or be

available to perform, a SSAA as a result of a drug or alcohol testing related

suspension event, the Club will only permit the employee to again begin

performing or being available to perform a SSAA in the following

circumstances:

(a) the employee has undergone a comprehensive assessment for drug or

alcohol use; ....





(9) Where the Club has not permitted a SSAA employee to ... (Cont’d)

(b) if the comprehensive assessment recommended the employeecommence a drug or alcohol intervention program, the employee hasbegun participating in a nominated drug or alcohol intervention program;

(c) the employee has given the Club a written undertaking to conform withthis program.

(d) A negative test will be required and the employee shall providesatisfactory evidence that the cause of the breach has been addressed.

(e) the employee is considered fit to resume performing, or being availableto perform, a SSAA by;

(i) a DAMP Medical Review Officer; and

(ii) the employee’s treating clinician, if any.

(f) If the suspension event related to a drug test and at the time theemployee was considered fit to resume SSAAs, the employee receivesa confirmatory drug test and records, for the test, a result that;

(i) was not a positive result; and

(ii) a DAMP Medical Review Officer is satisfied it indicates theabsence of testable drug use.

(10) Follow-up testing may be conducted within the one month period from thedate of return to SSAAs.

(11) The Club will permit a SSAA employee time to attend a nominated drug oralcohol intervention program, if;

(a) a DAMP Medical Review Officer has advised the Club that the employeeshould attend the program;

(b) the employee has given the Club a written undertaking to conform withthis program.

(12) Where drug or alcohol testing undertaken by a employee returns a positiveresult, the employee shall be required to reimburse the Club for the initial,confirmation, return to work testing and following-up testing. Any counsellingundertaken shall be at the employee’s expense.




10.9 SELF-REFERRAL

(1) An aim of this policy and the educational material available is to encourage

Club personnel to recognise problematic use of substances and to obtain the

assistance they need.

(2) Personnel seeking assistance from the DAMP Supervisor will be offered

assistance by way of counselling or other treatment. They may be provided

with flexible leave arrangements in order to complete any treatment /

rehabilitation program.

(3) Club employees or contractors may wish to seek assistance from an AOD

professional, independent of the employment arrangement established by the

Club.

10.10 ROLE OF THE MEDICAL REVIEW OFFICER

(1) The Club will consult a DAMP Medical Review Officer in the following

circumstances;

(a) If a drug test conducted under the program returns a positive

confirmatory drug test, to determine if the presence and level of a

testable drug detected by the test could be the result of legitimate

therapeutic treatment or some other innocuous source; and

(b) To review medical information concerning a person’s failure to give a

body sample for drug or alcohol testing because of a claimed medical

condition;

(c) To determine, in consultation with the employee’s treating clinician, if the

employee is fit to resume performing or being available to perform a

SSAA after being required to cease performing or being available to

perform SSAA for a drug or alcohol testing related incident.





10.11 DISCIPLINARY ACTION

(1) A Club employee who returns a positive result for a confirmatory drug test will

issued with a written warning.

(2) A Club employee shall be dismissed from Club employment where;

(a) an employee returns the second positive test result; or

(b) an employee returns a positive test result within the 3 month period

following a return to SSAAs after a suspension from SSAAs due to a

positive test result; or

(c) an employee refuses to give the Club a written undertaking to conform

with this program; or

(d) the employee does not undertake and complete a AOD rehabilitation

program when a DAMP Medical Review Officer has advised the Club

that the employee should attend the program.

(3) When unable to perform SSAAs for a period of time following a suspension

event related to a drug test, a Club employee shall be employed on non-

SSAAs.

10.12 PRIVACY, REPORTING AND RECORDS

(1) The Privacy Act 1988 may apply to information gathered under this program

and information held in relation to the outcomes of drug and alcohol testing,

whether conducted under the Club or by CASA.

(2) The Club will ensure it records and supplies the following information to

CASA within 21 days of 1 March and 1 September each year, or as otherwise

required by CASA;

(a) Drug and alcohol education;

(b) Drug and alcohol testing;

(c) Drug and alcohol response;

(d) The number of SSAA employees engaged; and

(e) Details of the current DAMP Contact Officer.

....




10.12 PRIVACY, REPORTING AND RECORDS

(3) Copies of the forms used to administer this DAMP are shown as Appendixes

to the DAMP.

(4) All records associated will drug and alcohol disciplinary processes will be

retained in employee files or contractor’s folder, as applicable.

(5) The information reported to CASA will not contain any additional detail,

beyond that required by CASR Part 99, which might identify individuals

employed by the Club, its contractors or subcontractors.

(6) Where requested to do so, the DAMP Contact will supply information about

the identity of a DAMP employee to a CASA approved tester within 1 hour of

such a request being made.

(7) The Club will keep all records pertaining to this DAMP that are used to

provide information to CASA for a period of 5 years. This information will be

kept in a secure location. Within 6 months of the expiry of the 5 year record

keeping period, the DAMP Supervisor will ensure such records are destroyed.

10.13 REVIEW, VARIATIONS, AUDIT AND COMPLIANCE

(1) The Club will review this program at regular intervals of at least every 5

years, or as directed by CASA, in order to ensure its continued compliance

with the requirements of the CASRs.

(2) To ensure the appropriate development, implementation and enforcement of

the Club’s program, CASA may audit the Club and require it to provide

relevant documentation.

(3) the Club may at any time be required by CASA to make specific changes to

this program, or to prepare a new program, to ensure ongoing compliance

with the CASRs.

(4) the Club may implement variations to this program from time to time and,

where relevant, will provide 3 months written notice to its employees setting

out these changes. At the end of the 3 months, the DAMP shall be revised to

incorporate the variations and a copy of the revision issued to all DAMP

holders.

‘



DRUG AND ALCOHOL MANAGEMENT PLAN Appendix 1

Page 1


DAMP AWARENESS TRAINING RECORD

NAME: ARN/LIC:

ADDRESS:

PHONE: DATE OF BIRTH:

EMPLOYER: POSITION:

Employees who perform or are available to perform a safety sensitive aviation activity (SSAA) are to complete this drug andalcohol awareness training before conducting a SSAA. Upon completion, this form is to be forwarded to the Club's DAMPSupervisor. Read or viewed insert U

TRAINING RESOURCES

CASA Fact Sheets CASA Interactive Quiz

* Alcohol “ * Interactive Quiz “

* Methamphetamine “ CASA Video

* Ecstasy (MDMA) “ * Educational video “

* PMA “ CASA Presentations

* Cannabis “ * AOD presentation “

* Cocaine “ Club DAMP “

* Opioids “ Testing in the Workplace “

* Codeine “

* Over-the-counter substances “ The CASA training resources are available on line athttp://aod.casa.gov.au/aod/resources/index.html

* Prescription medications “

I, certify that I have read and viewedthe above drug and alcohol educational resources.

Signature: Date:

DAMP Supervisor Signature: Date:




Page 1


EMPLOYEE’S DAMP RECORD

NAME: ARN/LIC:

ADDRESS:

PHONE: DATE OF BIRTH:

PRE-EMPLOYMENT TESTING

CONDUCTED BY: PHONE: TYPE: DATE:

URINE/ORAL

AOD TRAINING

CONDUCTED BY: DATE: CONDUCTED BY: DATE:




Page 2


EMPLOYEE’S DAMP RECORD

NAME: ARN/LIC:

AOD TESTING COMPLETED

CONDUCTED BY DATEREASON TYPE RESULT

R/PD/AI/RS* U/O* INITIAL CONFIRM’RY

* R= Random; PD= Pre-deployment; AI= Accident/Incident; RS = Reasonable Suspicion; U/O = Urine/Oral




Page 1


REASONABLE SUSPICION RECORD

NAME: ARN/LIC:

DETAILS OF GROUNDS FOR REASONABLE SUSPICION

DAMP SUPERVISOR: TIME (UTC) DATE

Reason:

AOD TESTING REQUIRED

Employee shall undergo drug and alcohol testing conducted by;

TESTING FACILITY PHONE TIME (UTC) DATE

EMPLOYEE SIGNATURE DAMP SUPERVISOR SIGNATURE

RESULTS OF AOD TESTING

CONDUCTED BY DATETYPE RESULT

INITIAL CONFIRM’RY

URINE/ORAL/BAC

A refusal to undertake AOD testing or tampering with the sample is grounds for removal from SSAA. Where the results of the AOD testing are positive, the employee shall undergo the Club Drug and Alcohol Response Program. The DAMP Supervisor shall complete DrugAnd Alcohol Response Program Record.




Page 1


DRUG AND ALCOHOL RESPONSE RECORD

NAME: ARN/LIC:

PHONE: DATE OF POSITIVE TEST:

POSITIVE CONFIRMATORY TEST RESULT

FIRST SECOND CROSS OUT NON-APPLICABLE

TESTING FACILITY PHONE TIME (UTC) DATE

ACTION TO BE TAKEN

If this is the second positive result under the Club's DAMP, a dismissal notice is to be issued to theemployee.

DISMISSAL ISSUED: YES / NO DATE: Attach copy

WARNING ISSUED: YES / NO DATE: Attach copy

The Club has been advised by that the employee attend a Drug and Alcohol Intervention Program conducted by

at Date: Time:

The employee has given a written undertaken to conform with this program and this undertaken hasbeen received by the DAMP Supervisor. Yes - No Attach copy

RETURN TO SSAA

Recommendation of DAMP MRO YES - NO AOD TESTING Negative

Returned to SSAA Date: Pre SSAA YES - NO

Three Month Period YES - NO




Page 1

TRAINING RESOURCES

The DAMP Supervisor shall utilise the following documentation and resources for thetraining of Club employees as required by sub-section 10.5.

Club DAMP

The following resources are available online athttp://aod.casa.gov.au/resources/index.html

CASA Fact Sheets

* Alcohol

* Methamphetamine

* Ecstasy (MDMA)

* PMA

* Cannabis

* Cocaine

* Opioids

* Codeine

* Over-the-counter substances

* Prescription medications

CASA Interactive Quiz

* Interactive Quiz

CASA Video

* Educational video

CASA Presentations

* AOD presentation

DAMP Supervisor Resources

For further information for the DAMP Supervisor refer to the “A Training Kit to Respondto Alcohol and other Drug Issues in the Workplace” This document is available online at;

• CASA web site

• National Centre for Education and Training on Addiction web site. ‘


© AEROSERVICE 2000

08/00 OPERATIONS MANUAL A-B(iii)

PART B

SPECIFIC AIRCRAFT OPERATING PROCEDURES

FOR

AEROPLANES

INDEX TO SECTIONS

TITLE SECTION

PREFACE PAGES BO

AIRCRAFT OPERATIONS B1

FLIGHT PLANNING AND PERFORMANCE B2

LOADING Reserved

ENVIRONMENTAL Reserved

SECURITY AND SURVIVAL B5


© AEROSERVICE 2000

08/00 PREFACE PAGES A-BO-3

0.1 INTRODUCTION

(1) This Part of the Operations Manual contains information and instructions to

assist flight crew members in the handling and operation of all aeroplanes not

exceeding 5700 kg MTOW that are specified in the Air Operators' Certificate

issued to THE REDCLIFFE AERO CLUB.

(2) The individual aircraft Flight Manual and the manufacturer's handbook for the

aeroplane in use together with the supplementary data contained in this Part

constitute the Specific Aircraft Operating Procedures. The manufacturer's

handbook (or an abbreviated version) is to form part of the aircraft's equipment

and the pilot in command is responsible for ensuring its carriage.

(3) Pilots are reminded that the operating data in the manufacturer's handbook

applies to the aeroplane type identified within that publication by model, year

of manufacture or serial numbering while the data in the approved Flight

Manual applies only to the specific aeroplane identified by the registration

letters and serial number stated in that document.

(4) All operating limitations, conditions and requirements of the individual aircraft

Flight Manual shall take precedence over any information contained in this

Part. See sub-section 1.11 of Section A1, Part A.

(5) Operation of a particular aeroplane is subject always to the pilot in command

being endorsed on type, appropriately rated and meeting the recency

requirements as specified at sub-section 2.7 of Section A2, Part A.GG



04/04 AEROPLANES A-B1-1

SECTION B1

AIRCRAFT OPERATIONS

SUB-SECTION PAGE

1.1 AIRCRAFT TECHNICAL DATA A-B1-3

1.2 NORMAL PROCEDURES A-B1-4

1.3 EMERGENCY PROCEDURES A-B1-6

1.4 CREW COMPLEMENT AND DUTIES A-B1-6

L 1.5 MINIMUM EQUIPMENT AND UNSERVICEABILITES A-B1-7

1.6 TAKE-OFF AND LANDING BY CO-PILOT Reserved

1.7 IN-FLIGHT ENGINEERING LOG Reserved

1.8 TAKE-OFF AND LANDING DATA Reserved




1.2 AIRCRAFT TECHNICAL DATA

(1) Particulars of the individual aircraft and its systems, including standard optional

equipment available at the time of manufacture and which may be installed in

the aircraft are described in the appropriate sections of the manufacturer's

handbook and/or maintenance and servicing manuals for that aircraft.

(2) For aeroplane general data, airworthiness limitations and data pertaining to any

optional equipment or modifications installed on the aircraft in use, refer to the

appropriate Sections of the approved Flight Manual for that aircraft.

(3) The recommended procedures for proper ground handling, routine care and

servicing of the aircraft and its equipment are described in the applicable

aircraft manufacturer's handbook and/or service manuals.

(4) The appropriate tables/charts and performance data, including graphs and

tables and other information which is to be used to facilitate the planning and

safety of flight and for the conducting of flight operations, are contained in the

appropriate sections of the manufacturer's handbook and Flight Manual for the

particular aircraft.

L (5) Except when using a factored performance chart, the take-off and landing

distance obtained from charts appearing in the manufacturers' handbooks for

Club operated aeroplanes shall be factored by 1.15 when used for determining

the take-off and landing distance required for a particular operation.

(6) The minimum runway width applicable to Club operated aeroplanes is 10

meters.



© AEROSERVICE 2000


1.3 NORMAL PROCEDURES

(1) General Requirements:

(a) Club aeroplanes shall at all times be operated in accordance with theoperating limitations and other essential operating data contained in theindividual aircraft Flight Manual.

(b) The operating procedures relating to any optional equipment, modificationor specialised function for which a particular aeroplane is approved, shallbe in accordance with the relevant limitations and instructions containedin the appropriate section(s) of the currently amended Flight Manual forthat aircraft.

(c) The pilot in command of a Club operated aeroplane shall ensure that alistening watch is maintained at all times from immediately prior to thetime at which the aeroplane commences to move for a flight until theaeroplane stops on the apron after a flight, or in the case ofcommunicating with an ATC unit, he/she shall personally maintain alistening watch at all times the aeroplane is under control of that ATC unitand shall comply with the instructions issued by ATC. Club pilots shalluse the radio telephony procedures and phases detailed in the AIP.

(2) Specific Requirements:

Notwithstanding anything else to the contrary, all flight crew members mustobserve the following specific requirements when piloting Club operatedaircraft:

(a) Reduced Power Take-offs shall at NO TIME be used.

(b) Power Reduction to climb power after take-off shall not be made at aheight less than 300 feet above the aerodrome elevation. The actualheight will vary according to traffic, terrain, gross weight, field elevationand temperature.

(c) Aeroplanes Shall be Climbed at not less than VYSE (blue line) (VY forsingle engine aeroplanes) until a safe height (at least 300 feet AGL) isreached unless a climb at not less than VX is required to clear obstacles.

....




1.2 NORMAL PROCEDURES

(2) Specific Requirements: (cont'd)

(d) All Approaches in Multi-engine Aeroplanes shall be made at a speed not

less than VYSE (blue line) (Vy for single engine aeroplanes) until a point

at which the pilot has decided he/she is committed for the landing, when

the airspeed adopted shall be not less than the airspeed calculated from

the approved landing weight chart in the individual aircraft Flight Manual.

(e) Flaps shall not be retracted until the aircraft has taxied clear of the

runway after landing.

(f) Avionics master switch shall be switched off prior to starting and prior to

shut down of engines. For aircraft not fitted with an avionics master

switch, each avionics unit will be individually switched off in that aircraft.

(g) Anti-collision Beacons shall, at night or in conditions of poor visibility, be

switched on before the engines have been started, and switched off after

the engines are shut down.

(h) Strobe Lights shall, at night or in conditions of poor visibility, be switched

on before entering runways and switched off after exiting runways. Strobe

lights may, at the pilot's discretion, be switched off in flight while

operating in cloud at night.

(i) Navigation Lights will be switched on at night and in conditions of poor

visibility.

(j) Auto Pilot will not be used below 1000 feet above ground level unless

specific permission has been given by the Chief Pilot or delegate.

(k) Combustion Type Cabin Heaters should not be operated below 1000 feet

AGL except to ensure passenger/pilot comfort in low temperature

conditions. However, the heater may be used on the ground to demist the

windscreen and ensure clear vision for the pilot during take-off.

L (l) The Club specifically prohibits the pilot in command of a Club aeroplane

from towing, dropping or picking up of any person or object while that

aeroplane is in flight.


© AEROSERVICE 2000


1.4 EMERGENCY PROCEDURES

(1) An emergency briefing is to be considered before every take-off, regarding theintentions of the pilot in command before/after committed point, and his/herintentions below LSALT at night. If a second pilot or an instructor is carried,the pilot flying is to verbally brief the pilot not flying of these intentions and ofany requirements or delegation of duties the pilot in command may wish to giveto that crew member.

(2) In the event of an engine failure, equipment malfunction, or aircraft emergency(including fire on the ground or in the air), the recommended proceduresdescribed in the Emergency Procedures section of the applicable aircraftmanufacturer's handbook shall be followed to deal with the particular problem.

(3) In addition to the actions detailed in 1.3(2) above, the pilot in command shalladvise ATS immediately giving all relevant information.

(4) For the emergency procedures applicable to any optional equipment installedin, or non-standard configurations approved for, a particular aeroplane refer tothe appropriate supplement in the Flight Manual for that aircraft.

(5) Pilots should appreciate the importance of transmitting a radio distressmessage at the earliest possible opportunity after the onset of an in-flightemergency.

(6) Manufacturers' handbooks for certain early model aeroplanes omit some or allemergency procedures. Should the Club be in the position of operating suchan aircraft, the Chief Pilot is to ensure that emergency procedures (includingfire procedures and electrical load reduction in the event of alternator/generatorfailure) not included are inserted in the applicable aircraft manufacturer'shandbook and are brought to the attention of all Club pilots.

1.5 CREW COMPLEMENT AND DUTIES

(1) The minimum operating crew required for each Club operated aeroplane shallbe one pilot or as specified in the individual aircraft Flight Manual. The pilotassigned on the Club’s roster to fly a particular aircraft as Captain shall be thepilot in command of that aircraft.

(2) The pilot in command shall occupy the left hand seat at all times except forFOIs, instructors or check pilots who may occupy the right hand seat.




L 1.6 MINIMUM EQUIPMENT AND UNSERVICEABILITES

L (1) CAR/CAO Minimum Equipment Requirements- IFR Operations

(a) Radio Apparatus

(i) minimum of one VHF radio and, if area of operations require the

carriage, one HF radio;

(ii) for operations OCTA, a minimum of one radio navigation aid. This

may be either one ADF or one VOR;

(iii) for CTA operations either DME or GPS and a minimum of one radio

navigation tracking aids. This may be one ADF or one VOR;

(iv) any other radio equipment that may be specified in the in the

individual aircraft Flight Manual for the class or type of operation in

which the aircraft is engaged.

(b) Instruments and Indicators

(i) Airspeed Indicator;

(ii) Altimeter;

(iii) Compass;

(iv) Directional Gyro;

(v) Turn and Slip Indicator;

(vi) Vertical Speed Indicator

(vii) Two Artificial Horizons;

(viii) Power Source Indicators for instruments (iv), (v) and (vii);

(ix) Outside Air Temperature Gauge;

(x) Pitot Heater;

(xi) Balanced Static Ports or Normal and Alternate Static Ports;

(xii) Time piece;

(xiii) any other instruments and indicators that are specified in the individual

aircraft Flight Manual.

(c) An assigned altitude indicator meeting the requirements specified in sub-

section 7 of CAO 20.18.

....





L (2) CAR/CAO Minimum Equipment Requirements- VFR Operations

(a) Radio Apparatus

(i) a minimum of one VHF radio and, if area of operations require the

carriage, one HF radio;

(ii) any other radio equipment that may be specified in the individual

aircraft Flight Manual for the class or type of operation in which the

aircraft is engaged.

(b) Instruments and Indicators

(i) Airspeed Indicator;

(ii) Altimeter;

(iii) Direct Reading Magnetic Compass;

(iv) Turn and Slip Indicator;

(v) Outside Air Temperature Gauge;

(vi) Time piece;

(vii) any other instruments and indicators that are specified in the individual

aircraft Flight Manual.

(3) Emergency Locator Transmitter

All Club operated aircraft shall be equipped with or carry a portable or fixed

ELT.

(4) Transponder

Except when operating in the circuit area at a GAAP aerodrome, all Club

aeroplanes shall be fitted with a Mode A/C transponder.

....





(5) Aircraft Lighting

The minimum lighting equipment for operations in Club aeroplanes at night

shall be;

(a) fixed instrument illumination for all instruments and equipment used by

the pilot for the safe operation of the aeroplane so that;

(i) the instruments and equipment are easily read or discernible;

(ii) it does not shine directly or indirectly on the pilot’s eyes;

(iii) an alternate source of power is immediately available in the event of

a failure of the normal source;

(iv) the intensity of the illumination can be controlled where required.

(b) two landing lights, except for non-passenger carrying charter operations

or aerial work operation, where one landing light is required;

(c) passenger compartment lights;

(d) adequate lighting in the pilot’s compartment to enable the reading of

maps and flight documents;

(e) navigation and anti-collision lights;

(f) a shock proof electric torch for each pilot.


....




1.5 MINIMUM EQUIPMENT AND UNSERVICEABILITES

(6) Unserviceabilities

(a) Charter Operations

L Except where permitted by the Operator Minimum Equipment List for the

particular aeroplane or where the Club has received an approval for the

flight, all instrumentation and equipment, except passenger convenience

items, fitted to Club aeroplanes engaged in charter operations shall be

serviceable prior to take-off.

(b) Aerial Work Operation

Where an aerial work operation is to be conducted with an unserviceable

instrument or equipment not required for that operation, the unserviceable

instrument or equipment shall be prominently placarded 'UNSERVICEABLE'.

The flight may also be conducted where the unserviceable instrument or

equipment is removed from the aeroplane after approval has been

obtained from CASA or a delegate under CAR 35 for that removal.

(c) Maintenance Release Endorsements

An endorsement shall be entered in Part 2 of the Maintenance Release

detailing the unserviceability and any restriction to the operation of the

aeroplane that results from that unserviceability.GG


© AEROSERVICE 2000


SECTION B2

FLIGHT PLANNING AND PERFORMANCE

SUB-SECTION PAGE

2.1 STANDARD FLIGHT PLANS Reserved

2.2 STANDARD ROUTE TIMES Reserved

2.3 STANDARD ROUTE FUEL LOADS Reserved

2.4 PERFORMANCE Reserved

2.5 POINT OF NO RETURN A-B2-3

2.6 CRITICAL POINT A-B2-3

2.7 LATEST DIVERT TIME/POINT A-B2-3

APPENDIXES

1. FLIGHT PLANNING DATA


© AEROSERVICE 2000


2.5 POINT OF NO RETURN

(1) The technique of flying to a point of no return (PNR) can be very useful in dayto day operations when the available fuel load is limited and/or headwinds areforecast It should not be the norm in planning but will often give an otherwiseunattainable sector distance.

(2) Club procedure is as follows:

(a) Flight plan to a suitable aerodrome on the intended route in the normalmanner. All standard flight fuel reserves must be carried. The aerodromeobviously must have fuel available and facilities for passengers. As thisaerodrome is approached, use the ambient conditions and remaining fuelon board to calculate a time to a PNR from this aerodrome towards theintended destination.

(b) When approaching the PNR replan the fuel required with reserves tocontinue from the PNR to the destination. In most cases if reasonablecalculations have been made at the planning stage the aim will be achievable.

(3) Time to PNR = Flight fuel (mins) x GS return / GS out + GS return

2.6 CRITICAL POINT

(1) There may be times when operating long distances and operating at nightwhen normal emergency strips are not available that it would be necessary toknow the sector equi-distance point.

(2) Distance to CP= Distance x GS return / GS out + GS return

2.7 LATEST DIVERT TIME/POINT

(1) No flight shall depart any station unless the pilot in command has ensured thatsufficient fuel is carried in the tanks so that no less than the minimum quantitiesspecified below will be on board upon arrival at the destination airport, or at thealternate airport if an alternate is required.

(2) If a successful approach and landing at the destination aerodrome appearsmarginal due to weather or any other reason, the pilot in command shalldetermine the latest divert time or position to proceed to a suitable alternate.The divert time/position shall be determined so as to allow the aeroplane toland at the alternate with the required fuel reserves intact.


© AEROSERVICE 2000


2.7 LATEST DIVERT TIME/POINT

(3) While enroute, should the pilot in command become aware that insufficient fuel

remains in the aircraft fuel tanks to ensure landing at the destination or

alternate airport with no less than the required fuel reserves, he or she shall

land at a suitable alternate airfield so as to have no less than the specified

minimum fuel on board after landing. If no suitable alternate airfield is

available, a fuel emergency shall be declared with ATS or if unable to make

contact with ATS a fuel emergency broadcast shall be made on area

frequency. Immediately that a fuel shortage is realised, the pilot in command

should adopt a power setting for the aircraft that will give maximum endurance.

Time to prepare for a forced landing due to fuel starvation should be taken if

a suitable airfield does not exist to divert to.

GG


01/09 THE REDCLIFFE AERO CLUB Section B2

FLIGHT PLANNING AND PERFORMANCE Appendix 1

Page 1

FLIGHT PLANNING DATA

AIRCRAFT TYPE

TOTAL USABLE FUEL LTRS

TAS

BLOCK

FUEL

FLOW

LTS/HR

POWER

4000 PH/ ISAMP/RPM

65%

OIL CAPACITY

US QTS

MAINS AUX TIPS MAX MIN

7GCAA 133 N/A N/A 115 33 2300 8 6

8KCAB 151 N/A N/A 120 40 25"/2500 8 6

Beech BE76 379 N/A N/A 140 76 24"/ 2300 8 6

Beech A36 281 N/A N/A 160 60 23"/2300 12 10

CA25N 48 N/A N/A 70 15 5000 3 2

Cessna 152 92 N/A N/A 95 25 2300 6 4

Cessna 172 189 N/A N/A 105 36 2400 6 4

Cessna 172SP(s) 201 N/A N/A 120 40 2300 8 6

Cessna 177 185.4 N/A N/A 120 40 23"/2450 8 6

Cessna 210M 336 N/A N/A 150 60 23"/2400 10 7

Cessna 310 386 242 158 189 110 23"/2400 12 9

Cessna U206G 334 N/A N/A 130 60 23"/2400 12 9

Cessna 182 334 N/A N/A 130 50 20"/2400 12 10

DH82 80 N/A N/A 80 30 1850 9 -

Grumman AA 5B 193 N/A N/A 122 40 2450 8 6

Piper PA32-300 356 N/A N/A 130 60 23"/2400 12 8

Piper PA28 182 N/A N/A 120 40 2450 8 6

Piper PA28 151 182 N/A N/A 105 26 2450 8 6

Piper PA30-160B 205 114 114 150 70 22"/2400 8 6

Piper PA38 113.6 N/A N/A 90 25 2350 6 4

Piper PA28R - 200 182 N/A N/A 130 50 22"/2400 8 6

PA31-350 378 303 N/A 160 163 30"/2300 12 6

PN68 389 N/A N/A 135 80 22"/2300 8 6

L PA44-180T 410 N/A N/A 150 84 27.5"/2400 6 5

L PA32-301RT 387 N/A N/A 154 75 30"/2300 12 11

For Club operated aircraft not listed above, the pilot in command shall use the fuel consumption tablesfrom the Performance Section of the particular Pilot's Operating Handbook.




SECTION B5

SECURITY AND SURVIVAL

SUB-SECTION PAGE

5.1 SECURITY FROM SABOTAGE A-B5-3

5.2 SECURITY FROM VANDALISM A-B5-4

5.3 SECURITY FROM UNAUTHORISED ENTRY A-B5-4

5.4 TIE-DOWN EQUIPMENT A-B5-4

5.5 WEATHER PROTECTION A-B5-4

5.6 MEDICAL KIT A-B5-4

5.7 SURVIVAL KIT AND SURVIVAL INSTRUCTIONS A-B5-5

5.8 MINIMUM EMERGENCY EQUIPMENT TO BE CARRIED A-B5-4




5.1 SECURITY FROM SABOTAGE

(1) Owners and operators are responsible for the security and safety of their ownaircraft, associated facilities and areas specifically allocated for their use at aparticular aerodrome.

L (2) To minimise the risk of sabotage away from base where hangarage is notavailable, the pilot in command should select an area that offers the bestsecurity protection available such as a lighted area or near an occupiedbuilding.

L (3) Pre-flight Security Checks

(a) The pilot in command must ensure that a pre-flight security check of aCompany aeroplane is carried out if;

(i) the proposed flight is the aeroplane's first flight since returning toservice after maintenance has been carried out outside a securitycontrolled airport; or

(ii) the aeroplane has not been hangared or continuously protected fromunauthorised access since its previous flight.

(b) This check shall include inspection of;

(i) the cabin which must be done before any passenger boards theaeroplane;

(ii) the cargo compartment which must be done before any cargo isloaded;

(iii) the baggage compartment(s) which must be done before anybaggage is loaded.

(c) This check must also include a comprehensive inspection of;

(i) the interior of the aeroplane; and

(ii) any unlocked storage compartment in any part of the aeroplane'sinterior; and

(iii) the parts of the aeroplane's exterior that are reasonably accessible,i.e. check propeller(s), pitot tube(s), doors, windows, tank caps, fuelvents and any other aperture for signs of tampering, forcible entry orthe presence of foreign matter.




5.2 SECURITY FROM VANDALISM

Take appropriate action in accordance with sub-sections 5.1(2) and 5.3, this Section.

5.3 SECURITY FROM UNAUTHORISED ENTRY

(1) Whenever a Club operated aircraft is left unattended in the open, the pilot in

command shall ensure that

(a) keys are removed; and

(b) windows, doors and hatches are adequately secured to deter

unauthorised persons from gaining entry; and

L (c) the aircraft locking device is fitted and the visual alert is displayed.

L (2) No member of the public shall be permitted to enter or look around the

aeroplane without a Club escort.

5.4 TIE-DOWN EQUIPMENT

Responsibility shall rest upon the pilot in command to ensure that the appropriate tie-

down equipment is either carried or will be readily available at the aircraft's

destination and used to secure the aeroplane when appropriate.

5.5 WEATHER PROTECTION

(1) Take action in accordance with sub-section 5.3 this Section and whatever

additional measures the pilot may deem advisable under the prevailing or

predicted weather conditions.

(2) The implementation of proper parking and tie-down procedures offers the best

protection against accidental damage to an aircraft from inclement weather

5.6 MEDICAL KIT

All Club aircraft shall be equipped with a first aid kit which meets the

recommendations of AIP/ERSA. It is the responsibility of the pilot in command to

ensure this kit is in its correct stowage location prior to flight.




5.7 SURVIVAL KIT AND SURVIVAL INSTRUCTIONS

(1) A survival kit, which meets the recommendations of AIP/ERSA and is

appropriate to the area to be overflown, will be carried on all flights within or

through a remote or sparsely inhabited area and on such other flights as the

Chief Pilot considers necessary and directs.

(2) Consideration should be given to the carriage of supplementary drinking water

to guard against dehydration when operating in high temperature conditions or

the planned route is over inhospitable terrain.

L

5.8 MINIMUM EMERGENCY KIT TO BE CARRIED

The minimum emergency equipment to be carried on Club aeroplanes shall consist

of

- First aid kit as per sub-section 5.6 this Section

- Fire extinguisher

- an Emergency Locator Transmitter.GG


© AEROSERVICE 2000

08/00 OPERATIONS MANUAL D(iii)

PART D

SPECIALISED OPERATIONS

INDEX TO SECTIONS

TITLE SECTION

GENERAL CONDITIONS DO

LOW FLYING TRAINING D1

AERIAL SPOTTING D2

AERIAL SURVEYING D3

FILMING AND PHOTOGRAPHY D4

UNDERGROUND UTILITIES INSPECTION D5

POWERLINE INSPECTION D6


© AEROSERVICE 2000

08/00 SECTION DO DO-1

GENERAL CONDITIONS

0.1 CIVIL AVIATION REGULATION REQUIREMENTS

(1) For the purposes of sub section 27(9) of the Civil Aviation Act 1988,

commercial purposes are defined by CAR 206.

(2) The specialised operations detailed in Part D of this Operations Manual are

prescribed as Aerial Work purposes in accordance with sub section (1)(a) of

CAR 206;

(3) Pilots are reminded, however, that the primary categorisation of a flight may be

in fact be charter, as prescribed by CAR 206(1)(b), in which case, the

provisions of Part D of this Manual do not apply and the flight may not be

conducted in accordance with these provisions. For example, flight below 500

ft AGL is not authorised and the conditions detailed in the CASA Approval

issued in pursuance of CAR 157 (i.e. the "Company's Low Flying Permit, refer

to sub-section 1.2 of Section A2, Part A1") do not apply.

(4) Commonsense must nevertheless be applied at all times to ensure that

bona-fide charter passengers are not exposed to the additional risks which

accompany low level flight. Bona-fide aerial work passengers and crew, i.e.

operators of fixed-in-aircraft cameras, are generally aware of these risks,

whereas others may not be. The mere fact, for example, that a charter

passenger may be carrying a camera (even a sophisticated camera) or, in fact,

that the person may be a professional photographer, does not automatically

imply that the nature of a particular charter flight may be altered to make the

flight an aerial work flight. Accordingly, flight at altitudes lower than those

associated with normal charter operations (ie not below 500 ft AGL) is NOT

authorised in these circumstances.

(5) In addition, passengers who are carried in the course of a normal aerial work

operation, as prescribed In Part D of this Manual, shall be clearly briefed

before flight that the operation is aerial work and not charter and that the

compulsory seat liability insurance as required by CASA for charter

passengers is not applicable to the operation.

....


© AEROSERVICE 2000


GENERAL CONDITIONS

0.2 PILOT RESPONSIBILITIES

(1) A Company pilot shall not fly as pilot in command of an aeroplane on anyspecialised operation unless:

(a) he/she is appropriately licensed and has the necessary pilotqualifications to perform the particular operation;

(b) permission has been obtained for any such task requiring an exemptionagainst a Civil Aviation Regulation; and

(c) the aeroplane concerned is approved for such use and is appropriatelyequipped for the task.

(2) Before engaging in a specialised operation, the pilot concerned shall ensurethat he/she is fully conversant with any dispensations or exemptions againstCARs and CAOs and/or operational specifications which may apply to theparticular task. Refer to sub-section 1.2 of Section A1, Part A.

(3) The pilot in command shall ensure that permission has been obtained from therelevant landowners before conducting low flying operations.

0.3 USE OF SEAT BELTS AND SAFETY HARNESS

(1) While conducting specialised operations, a crew member shall at all times beseated with his/her seat belt fastened except under the following conditions;

(a) While the aeroplane is operating above 1000 AGL, the crew membermay be restrained by a safety harness attached to a dispatcher’srestraint strap, in place of a seat belt; or

(b) The Company is in possession of a Direction issued under CAR 251(3)which allows the use of a safety harness attached to a dispatcher’srestraint strap, in place of a seat belt during operations below 1000 feetAGL. Refer to sub-section 1.2, Section A1 of Part A for any applicableDirection.

(2) The safety harness must conform to the relevant requirements of CAO Part108, "Specification - Aircraft Safety Belts, Safety Harnesses and Inertia Reelsand the dispatcher’s restraint strap must conform to the relevant requirementsof ASTO-C1001."


© AEROSERVICE 2000


GENERAL CONDITIONS

0.4 LOW FLYING APPROVAL

(1) Except as provided for in relevant Civil Aviation Orders, a Company aeroplane

shall not engage in any specialised operations involving flight at a lower height

than 500 feet above ground level unless, as required by CAR 157(4)(b), the

Company is in possession of a general permit for all flights or a specific permit

for a single flight to be made at the lower height and the pilot has the

necessary low flying qualifications..

0.5 AIRCRAFT OPERATION

(1) Flight with any door, window or other panel of the aeroplane open, removed

or modified, or with any special function equipment fitted, is not permitted

unless provision is made in the individual aircraft Flight Manual for operation

with the particular door, window or panel open, removed or modified, or with

the special equipment fitted, as the case may be

(2) The pilot in command shall ensure that fuel selectors are selected to 'BOTH' or

'MAINS' and the auxiliary fuel pumps selected 'ON' while engaged in low flying

operations.

0.6 CARRIAGE OF PERSONS

(1) A Company aeroplane engaging in specialised operations shall not carry any

person other than a person who is essential to the successful conduct of the

operation subject to the pilot in command being satisfied that the person on

board will not jeopardise the safety of the aeroplane at any stage of the operation.

(2) The pilot in command shall fully brief all passengers on the conduct of the

particular specialised operation in which they are engaged.

0.7 TOWING, DROPPING OF ARTICLES ETC.

Except when conducting operations in accordance with this Part, the Company

specifically prohibits the pilot in command of a Company aeroplane from towing,

dropping or picking up of any person or object while that aeroplane is in flight.


© AEROSERVICE 2000


GENERAL CONDITIONS

0.8 LOW LEVEL OPERATIONS

The following should always be kept in mind:

(1) The pilot's singular responsibility is to control the aeroplane and ensure that

the maximum degree of safety is maintained throughout all phases of the

operation, therefore, the pilot may cancel or terminate a flight at any stage if

he/she considers that it is not prudent to continue due to adverse weather or

other factors affecting safety.

(2) Company pilots shall obtain and study topographical charts for the intended

area of operations and shall pay particular attention the location of obstacles

that may hazardous to the intended operation.

(3) Transit flying during any specialised operation shall not be conducted below

500 feet AGL.

(4) Before descending to conduct low level operations, the pilot in command shall

conduct a reconnaissance of the area and identify the hazards noted from the

study of the charts and to make a note of other hazards not indicated on the

charts.

(5) Maintain a constant look-out for objects such as dead trees, telephone andpower lines, masts, towers and aerials (all of which are difficult to see againstthe landscape), large birds of prey and/or flocks of smaller birds particularlyin the early morning and late afternoon periods, or if in the vicinity of any placesuch as wooded hilly areas, water holes, permanent camp sites, etc. that arelikely to attract birds.

(6) In all instances other than when over flat terrain, it is recommended that the pilot

adopt the same technique as for flight in bad visibility and reduce airspeed to the

lowest safe cruise speed applicable to that aeroplane.

(7) Care should be exercised when rising terrain is encountered, that it does not

exceed the maximum climbing performance of the particular aeroplane. Under

no circumstances must the pilot attempt to out climb sharply rising terrain.

(8) The pilot must be constantly aware of the direction and speed of the surface

wind and the possibility of encountering differing local winds, downdraughts,

etc. caused by contrasting terrain features. ....


© AEROSERVICE 2000


GENERAL CONDITIONS

0.8 LOW LEVEL OPERATIONS

The following should always be kept in mind: (Cont’d)

(9) The pilot could also fall victim to the illusions created by drift near the groundwhen the surface wind is other than light and variable. Remember that:

(a) flying into wind will produce a noticeable reduction in ground speed;

(b) when flying downwind under certain conditions, the increase in groundspeed may be so noticeable that the pilot could be tempted to reduceindicated airspeed with disastrous results;

(c) when the wind is strong enough to produce a drift, turns are deceptive.For example

- when turning downwind from into wind, the aeroplane gives theimpression of slipping-in; and

- when turning into wind from downwind, the aeroplane appears to skidout.

WARNING

Low level turns must always be correctly executed in spite of the deceptiveappearance of the ground (although the drift is real) and because of thisphenomenon, the pilot must be especially careful to allow sufficient roomwhen turning from downwind to into-wind in a confined manoeuvring area.

0.9 OVERWATER OPERATIONS

(1) There are special problems associated with flying low over water. lf the waterit rough, height can be judged with fair accuracy, but when flying over a calm,glassy sea or expanse of water, particularly in hazy condition, the judgementof height can be very difficult and there may be little or no virtual differencebetween 50 and 250 feet. Water spray, in particular salt water spray. on thewindscreen can reduce visibility considerably.

(2) The aneroid altimeter is unreliable as a height reference and therefore the useof a radio altimeter, if fitted, it of major assistance in height control

(3) All persons on board a Company aeroplane conducting operations under thisPart are required to wear life jackets at all times when operating over water.

GG


© AEROSERVICE 2000

08/00 SECTION D1 D1-1

LOW FLYING TRAINING

1.1 APPROVAL TO CONDUCT LOW FLYING TRAINING

Low flying training may only be carried out by a pilot who has been approvedin writing by the Civil Aviation Safety Authority to conduct low flying trainingof other pilots in aeroplanes.

1.2 TRAINING OBJECTIVES

The object of this low flying training syllabus is to carry out the appropriate lowflying training of Company pilots, who are to conduct those specialisedoperations outlined in this Part of the Company's Operations Manual whichinvolve low flying operations.

1.3 AERONAUTICAL EXPERIENCE

(1) Before the issue of a Low Flying Training Certificate, a Company pilotundergoing low flying training in an aeroplane must;

(a) have a valid commercial or higher category pilot (aeroplane) licence;

(b) complete a minimum of five hours low flying training in aeroplanes withina period of ninety days and in accordance with the syllabus of trainingoutlined in paragraphs (6) and (7) of this Section.

(c) In the case of a pilot who holds or has held an agricultural rating inaeroplanes for which approval is sought, the requirement to undergo thelow flying training specified at sub-section 1.3(1)(b) may be waived,subject to the satisfactory completion of a flight test with a FlyingOperations Inspector or an approved pilot to demonstrate his/herproficiency in low level flying and emergency flight manoeuvres inaeroplanes.

1.4 CERTIFICATE OF COMPETENCY

Upon satisfactory completion of the low flying training specified at sub-section1.3(b) above, the approved pilot who conducted the training shall complete the LowFlying Training Certificate, a copy of which is shown at Appendix 1 to this Section.

1.5 LOW FLYING TRAINING

The five hours dual training is to be conduced by a pilot approved to conduct lowflying training in aeroplanes. Flying training is to be supplemented by groundbriefings. ....


© AEROSERVICE 2000


LOW FLYING TRAINING 1.6 GROUND BRIEFING

Before commencing flying training to conduct low flying operations, the trainee pilot

shall be briefed on the following;

(1) Height Perception - Pilots should be aware of the perception of height can be

extremely difficult at low level in the following conditions;

(a) calm water;

(b) sloping ground;

(c) flying into the sun when it is low on the horizon;

(d) areas of reduced visibility.

(2) Pilots should be aware that manoeuvring at low level in the following

conditions may lead to unintentional loss of height or a loss of control;

(a) in areas of reduced visibility e.g. precipitation, fog, smoke, dust or

industrial pollution;

(b) gusty or strong windy conditions;

(c) the attention of the pilot being distracted.

(3) Limitations of Pressure Altimeters - Pilots should be aware of the following

limitations of pressure altimeters;

(a) height tolerance for approval of altimeters used under the IFR and VFR;

(b) tolerance on the area QNH;

(c) method of checking of altimeters before departure.

(d) Radar Altimeters

(i) use of radar altimeters;

(ii) limitations of radar altimeters;

(iii) use and setting of the decision height feature.

....


© AEROSERVICE 2000


LOW FLYING TRAINING

1.7 TRAINING SYLLABUS - AEROPLANES

(1) Aeroplane Handling - to be conducted at a safe height:

The training for aeroplanes shall be in accordance with the following syllabusand is to be supplemented by ground briefing as necessary.

(a) level, climbing and descending turns up to 600 angle of bank;

(b) review of stalling symptoms and recovery in both wings level and turningflight up to 600 angle of bank;

(c) slow flying (including use of flap and the effect of changing flap settings);

(d) methods of losing height;

(e) manoeuvring at varying airspeeds and angles of bank.

(2) Low Flying - to be conducted only after the trainee pilot has demonstratedhe/she can perform safely sequences in 1.7(a), (b) and (c) above.

(a) low flying (below 100 feet above ground level);

(b) slow flying (including the use of flap);

(c) effects of wind (apparent change in speed while flying in head/tail windsand the apparent slip or skid in cross winds);

(d) action in the event of engine failure at low level;

(e) methods of losing height;

(f) procedure turns, steep and climbing turns from a fixed reference combinedwith descending turns back to the reference. The obstructed visibilityinherent in manoeuvring high-wing aeroplanes in descending turns to afixed ground reference shall be demonstrated;

(g) low flying in hilly terrain;

(h) effect of false horizons;

(i) effect of the sun, under certain conditions, on visibility; and

(j) approach to high ground - use of escape routes.GG.

© AEROSERVICE 2000

08/00 THE REDCLIFFE AERO CLUB Section D1

Appendix 1

Page 1


LOW FLYING TRAINING CERTIFICATE

This is to certify that

holder of pilot licence type ARN

has completed hours low flying training in aeroplanes as

Date Signed

(NAME IN BLOCK LETTERS)

Approved Pilot

Licence No


© AEROSERVICE 2000


AERIAL SPOTTING

2.1 GENERAL

(1) This Company may, from time to time, carry out aerial inspection and spottingoperations involving various tasks such as -

• the aerial inspection or surveillance of properties, water courses,irrigation systems, forest areas, etc;

• inspecting construction sites, fencelines, boundary markers and accessroutes;

• spotting and/or counting wildlife, domestic herds, etc.;

• checking abundance or lack of stock feed, water reserves, spread ofweeds;

• pest and vermin infestation/contamination;

• aerial surveillance of rivers, estuaries and other waterways;

• searching for lost or stranded persons/vehicles/boats;

• fire spotting, but not fire control

• marine and environmental

- and other tasks of a like nature on behalf of landholders, GovernmentDepartments/Agencies/Instrumentalities and other authorities.

(2) All spotting operations shall be flown in visual meteorological conditions andin accordance with the relevant Civil Aviation Regulations, flight rules andairway procedures unless concessional approval has been granted.

(3) Pilots should be constantly aware of the following manoeuvring hazards at lowlevel likely to result in loss of height or loss of control:

(a) turning with an ill defined horizon, e.g. in precipitation, fog or smokehaze;

(b) momentary distraction of the pilots attention, particularly during turns;

(c) manoeuvring in strong gusty wind conditions.

(4) Before embarking on an aerial spotting flight, the pilot in command shallensure that the requirements of Section DO this Part which are relevant to theparticular operation will be complied with.

(5) No person shall be carried other than a person essential to the successfulconduct of the operation. ....


© AEROSERVICE 2000


AERIAL SPOTTING

2.2 PILOT’S RESPONSIBILITIES

(1) to commencement of the sortie, the pilot in command shall ensure that:

(a) he/she has gained a proper understanding of the customer'srequirements;

(b) all concerned are in agreement with the proposed plan of action; and

(c) those persons involved in the particular mission including observers andground parties (if any) are adequately briefed on their duties, the signalsto be used, the general conduct of operations and safety precautions tobe observed.

(2) It is emphasised that ultimately the sole authority for the safety of theoperation is the pilot in command who may cancel or terminate a sortie at anystage if he/she considers that it is not prudent to continue due to adverseweather or other factors affecting safety.

2.3 PILOT QUALIFICATIONS

(1) The pilot in command of an aeroplane carrying out low level aerial spottingoperations must;


(b) hold an appropriate agricultural rating and approval to conduct low flyingoperations; or

(c) hold mustering approval for aeroplanes or have completed the dualtraining in accordance with the syllabus of training specified insub-section 1.6 and 1.7 of Section D1, with certification in accordancewith sub-section 1.4 of Section D1.

2.4 LOW FLYING PERMIT

If low level spotting operations are required, the pilot in command shall ensure thatthe Company is in possession of a general permit for all spotting operations or aspecific permit for a single spotting flight to be made at the lower height as requiredby CAR 157(4)(b).

2.5 BUSHFIRES

Pilots are to be aware of the danger of disorientation in the conditions of poorvisibility associated with bushfires. They are also to be aware of the effect ofextreme turbulence associated with operations in the vicinity of bush fires.

GG


© AEROSERVICE 2000


AERIAL SURVEYING

3.1 GENERAL

(1) From time to time a Company aeroplane may be utilised to conduct low-level

geographical, seismological marine or environmental survey flights or other

tasks of a like nature.

(2) All surveying operations shall be flown in visual meteorological conditions and

in accordance with the relevant Civil Aviation Regulations, flight rules and

airways procedures unless approval has been granted against a Regulation

or Order by the CASA.

(3) Before embarking on such a mission, the pilot in command shall ensure that

the requirements of Section DO this Part which are relevant to the particular

operation will be complied with.

(4) Before departure from base, the pilot shall ensure that he/she has gained a

proper understanding of the requirements, that all concerned have reached

agreement on the proposed plan of action and any person carried in the

aeroplane is adequately briefed on the conduct of operations and safety

precautions to be observed.

(5) No person shall be carried other than a person essential to the successful

conduct of the operation.

(6) During operations with door, hatchway or window removed, seat belts will be

worn continuously by all occupants. Any unused seat belts or cargo straps

must be secured and no loose articles are permitted in the aeroplane.

(7) The limitations and requirements imposed by the particular aeroplane's Flight

Manual supplement for operation with door, hatchway or window removed must

be observed.

(8) It is stressed that the aeroplane must at all times be loaded within C of G and

all up weight limitations compatible with the area of operation.

(9) When the task calls for the collection of samples in the field, suitable scales

will be carried in the aeroplane for weighing the objects before they are loaded

in the aeroplane.

....


© AEROSERVICE 2000


AERIAL SURVEYING


(1) Before an aeroplane uses any place as a landing area, the pilot in command

shall take all reasonable steps to ensure that:

(a) the dimensions of that place, surface strength and condition, including

height of grass and other vegetation, will permit safe landing and take-

off;

(b) the ALA is clear of all objects and animals likely to be a hazard in

manoeuvring the aeroplane.

(2) The pilot's singular responsibility is to control the aeroplane and ensure that

the maximum degree of safety is maintained throughout all phases of the

operation, therefore, the pilot may cancel or terminate a flight at any stage if

he/she considers that it is not prudent to continue due to adverse weather or

other factors affecting safety.


(1) The pilot in command of an aeroplane carrying out low level aerial surveying

operations must;


(b) hold an appropriate agricultural rating and approval to conduct low flying

operations; or

(c) hold mustering approval for aeroplanes or have completed the dual

training in accordance with the syllabus of training specified in

sub-section 1.6 and 1.7 of Section D1, with certification in accordance

with sub-section 1.4 of Section D1.


If low level surveying operations are required, the pilot in command shall ensure

that the Company is in possession of a general permit for all surveying operations

or a specific permit for a single surveying flight to be made at the lower height as

required by CAR 157(4)(b).

....


© AEROSERVICE 2000


AERIAL SURVEYING

3.5 BRIEFING

(1) When customer requirements involve the positioning and/or relocation of

personnel, goods and equipment, such flights are classified as charter and the

pilot in command shall ensure that all passengers are adequately briefed on

the conduct of that operation and the precautions that should be taken to

ensure their safety and well being. This briefing will include

- the need for sturdy boots and adequate clothing for the conditions likely

to be encountered;

- the care and welfare of any persons who may have to remain at a field

camp due to weather, mechanical failure or other circumstance that may

disrupt the planned operation;

- correct method of embarking and disembarking and other safety

requirements to be observed at landing sites;

- peculiarities and dangers associated with loading/unloading aeroplanes

e.g. the need for long objects (regardless of weight) to be handled by

two persons to avoid the possibility of damage to the aeroplane;

- procedures to be followed in the event of a forced landing;

- survival.GG


© AEROSERVICE 2000


FILMING AND PHOTOGRAPHY

4.1 GENERAL

(1) Photographic flights may be either air to ground or air to water utilising hand

held equipment. The images may be still or motion and recorded on flim or

video. As this type of flying is extremely demanding all such operations shall

only be conducted in visual meteorological conditions by day and in

accordance with relevant Civil Aviation Regulations, flight rules and airways

procedures.

(2) The camera operator shall at all times be seated with his/her seat belt or

harness fastened. The camera operator may be restrained to a safety harness

in lieu of a seat belt in accordance with the conditions specified in sub-section

0.3 of Section DO.

(3) At no time shall any part of the camera operator be outside the aeroplane

unless he/she is attached to the dispatcher harness.

(4) Photographic flights will be conducted only when satisfactory communications

can be maintained between the pilot and the camera operator.

(5) The limitations and requirements imposed by the particular aircraft flight

manual supplement for operation with door, hatchway or window open or

removed must be strictly observed. Any unused seat belts or cargo straps

must be secured and no loose articles are permitted in the aeroplane.

(6) Before embarking on a photographic flight, the pilot in command shall ensure

that the requirements of Section DO this Part which are relevant to the

particular operation will be complied with.


(1) The pilot in command is responsible for ensuring that any operation or

procedure is safely conducted within normal aeroplane operating parameters.

(2) When engaged on a filming sortie, the pilot in command is not absolved from

any action brought against him/her under common law in respect of noise,

damage to property or injuries to persons caused by such operations.

....


© AEROSERVICE 2000




(1) The pilot in command of a aeroplane carrying out low level filming or

photography operations must;


(b) hold an agricultural rating for aeroplanes and approval to conduct low

flying operations; or




with sub-section 1.4 of Section D1;

(2) Where aeroplanes are required to be flown in close proximity to each other the

pilots involved shall be competent in formation flight in accordance with

paragraph 2(a) of sub-section 6.9, Section A6, Part A.


If low level filming or photography operations are required, the pilot in command

shall ensure that the Company is in possession of a general permit for all filming or

photography operations or a specific permit for a single filming or photography flight

to be made at the lower height as required by CAR 157(4)(b).

4.5 FLIGHT PLANNING AND RADIO COMMUNICATIONS

(1) Speedy action is often the essence in filming and photography operations.

Pilots must be capable of planning their flights with minimum delay and should

at all times carry essential information and have a general knowledge of their

local town or city, surrounding areas and any salient features. Details of

countryside, mountains, hills, obstructions, powerlines, radio masts, danger

and prohibited areas are paramount.

(2) Normal ATS communications for aerial work operations will be observed.

When operating at low level the pilot should not rely on VHF. Plan the use of

HF whenever possible and thereby preclude having to interrupt filming so that

radios can be sorted out or communications re-established.

....


© AEROSERVICE 2000



4.5 FLIGHT PLANNING AND RADIO COMMUNICATIONS

(3) During formation or air to air photography, radio communications shall at alltimes be maintained between aeroplanes and where applicable, between ATSand the aeroplanes. Should a radio failure occur while the sortie is inprogress, this shall be indicated to the formation leader or by the formationleader to the other aeroplanes by pre-arranged visual signals. The operationwill terminate immediately. This may necessitate a formation leader change,which would be carried out in accordance with the pre-flight brief on loss ofcommunication procedure.

4.6 EQUIPMENT

(1) It is essential that the pilot in command has a working knowledge of the filmingapparatus to be used.

(2) Any camera mounts must be approved by the Civil Aviation Safety Authorityand must comply with the provisions of the particular aircraft Flight Manual.

4.7 SAFETY PRECAUTIONS AND EMERGENCY PROCEDURES

(1) The pilot in command, or formation leader if more than one aeroplane isinvolved, shall conduct a briefing of all persons concerned, covering allaspects of safety and aeroplane emergencies, with special emphasis on lowaltitude emergencies. It is particularly important to conduct a thoroughbriefing for the camera operator.

(2) The camera operator shall wear a seat belt or approved safety harness at alltimes. The safety harness should be attached to the securing lanyard at oneof the attachment points at the side of the harness. A safety line or lanyardfrom the camera shall be attached to an acceptable hard point in theaeroplane.

(3) The pilot in command shall conduct a thorough briefing on all emergencyprocedures including the operation of seat belts/safety harnesses, doors andemergency exits.

(4) It is emphasised that ultimately the sole authority for the safety of theoperation is the pilot in command who may cancel or terminate a sortie at anystage because of adverse conditions or other factors affecting safety.

....


© AEROSERVICE 2000



4.8 AIR TO AIR PHOTOGRAPHY

(1) Where an operation involves two or more aircraft flying in formation, whereapplicable, prior arrangements must be made with, and notification given to, AirTraffic Service. In conducting the operation, pilots concerned shall adherestrictly to the arrangements and conform to any instructions given by ATS.

(2) Normal aeroplane formation procedures shall be observed throughout, whilesafe lateral separation shall be maintained by means of visual contact.

(3) One pilot shall be nominated as pilot in charge of the operation and formationleader and that pilot shall be responsible for briefing the other pilot(s), thecamera operator(s) and any ground personnel taking part in the sortie. Thebriefing must clarify

(a) the take-off and landing sequence;

(b) airspeeds to be used for climbing, cruising and descending;

(c) any manoeuvres which will form part of the sequence;

(d) altitude at which the operation is to be conducted;

(e) radio procedures between aeroplanes, and between the aeroplanes andAir Traffic Service;

(f) procedure to be followed should radio contact between the aeroplanesbe lost.

4.9 AIR TO SURFACE PHOTOGRAPHY

(1) An aerial reconnaissance over the proposed area of operation is essential,particularly if the intention is to photograph moving objects (cars, speedboats,etc.), to check for obstructions such as power lines and such like, and tocheck wind direction as the pilot's attention will mostly be directed at thesubject during filming.

(2) When the intention is to photograph moving objects, a prior briefing must takeplace between the pilot, camera operator and the person(s) in control of themoving object(s). Air to ground communication is to be utilised for this typeof operation.

(3) Care must be taken to stay within the confines of the area checked on the pre-sortie flight. Persons involved in the ground or water part of the operation donot, in most cases, appreciate the complexities of conducting a photographicflight at low level.

(4) Photographic operations close to a residential area should be completed inthe shortest, safest possible time to reduce the noise irritation. GG


© AEROSERVICE 2000


UNDERGROUND UTILITIES INSPECTION

5.1 GENERAL

(1) Underground utilities inspection means the regular aerial inspection of

underground utilities on behalf of oil, gas, water or communication authorities

or companies for general condition, signs of leakage, or damage.

(2) The observer carried shall be a suitably qualified person who has been

selected by the organisation concerned and is acceptable to the pilot in

command of the aircraft.

(3) The pilot in command and the observer shall confer with the engineer in

charge or delegate and agree on all salient aspects of the operation,

identifying all major obstructions and establishing the location and direction

of the particular utility that is to be inspected.

(4) All utility inspections shall be flown in visual meteorological conditions and in

accordance with the relevant Civil Aviation Regulations, flight rules and

airways procedures.

(5) Before embarking an a utility inspection flight, the pilot in command shall

ensure that the requirements of Section DO this Part which are relevant to the

particular operation are complied with.


(1) The pilot in command of a Company aeroplane carrying out low level utilities

inspection operations must:


(b) hold an appropriate agricultural rating and approval to conduct low flying

operations; or




with sub-section 1.4 of Section D1.

....


© AEROSERVICE 2000


UNDERGROUND UTILITIES INSPECTION


If low level utility inspections are required, the pilot in command shall ensure that the

Company is in possession of a general permit for all utility inspection operations or a

specific permit for a single utility inspection flight to be made at the lower height as

required by CAR 157(4)(b).

5.4 PILOT RESPONSIBILITY

(1) The pilot's prime responsibility is to fly the aeroplane and ensure the maximum

degree of safety is maintained throughout the operation. The following

procedures must be adhered to:

(a) Do not attempt to observe or assist the observer other than to ensure the

aircraft is correctly positioned.

(b) Carry out early morning or late afternoon operations 'down sun' or wait

until the sun is in a more favourable position.

(c) Utilities located in sharply rising terrain or traversing steep slopes shall

be inspected on downhill runs, and then only if the pilot in command is

able to establish that there is a satisfactory escape route for the aircraft

on completion of the downhill run.

(d) Maintain a constant watch for overhead cables transiting or in close

proximity to the utility, particularly in areas of undulating terrain.

(e) In all instances other than when over areas of flat terrain, adopt the

same technique as for flight in bad visibility and reduce airspeed to the

lowest safe cruise speed specified for the aircraft.

(f) Seat belts shall be worn continuously by all occupants. An observer may be

attached to a safety harness in lieu of a seat belt in accordance with the

conditions specified in sub-section 0.3 of Section DO.

(2) The pilot in command of the aircraft may suspend or terminate the sortie at

any time in the interests of safety.GG


© AEROSERVICE 2000


POWERLINE INSPECTION

6.1 DEFINITIONS

* Powerline Inspection means the inspection of power transmission conductors,insulators, earthwires, connectors and poles for breakage or damage.

* Powerline means a line of poles supporting a conductor or number of conductors.

* Pole means a post or tower, or an array of posts and/or towers supporting aconductor or number of conductors.

* Conductor means a tube, cable or group of cables and the associated insulatorsand connectors used for the transmission of power from one place to another.

6.2 CONDITIONS

(1) The aerial inspection of powerlines and associated equipment on behalf ofelectrical generating and/or distribution authorities may only be carried out bya Company aircraft provided:

(a) the requirements of Section DO this Part which are relevant to theparticular operation are complied with; and

(b) any equipment which may be carried to assist with the inspections, suchas an Infra-red Camera, will not interfere with the aircraft radio systems.


(1) The pilot in command of a Company aeroplane carrying out low level pipelineinspection operations must;

(a) hold a current Commercial or higher category (aeroplane) pilot licence;and

(b) hold an agricultural rating for aeroplanes and approval to conduct lowflying operations; or

(c) hold mustering approval for aeroplanes or have completed the dualtraining in accordance with the syllabus of training specified insub-section 1.6 and 1.7 of Section D1, with certification in accordancewith sub-section 1.4 of Section D1.

....


© AEROSERVICE 2000




If low level powerline inspections are required, the pilot in command shall ensurethat the Company is in possession of a general permit for all powerline inspectionsor a specific permit for a single powerline inspection flight to be made at the lowerheight as required by CAR 157(4)(b).

6.5 OBSERVERS

Only those persons essential to the conduct of the operation shall be carried in theaircraft on powerline inspections. The observer shall be a person who is suitablyqualified (preferably a Line Foreman or equivalent) and has been selected by theElectricity Authority concerned and is acceptable to the pilot in command.

6.6 BRIEFING

The pilot in command and observer shall confer with the Distribution Engineer ordelegate and agree on all salient aspects of the operation and, from the Authority'spower distribution diagrams, identify all major obstructions including powerlines ofanother Authority transiting their area and establish the location and direction of theparticular powerlines or sections of powerline that are to be inspected.

6.7 OPERATION

(1) All inspection flights shall be carried out in visual meteorological conditionsand the pilot in command must adhere to the following procedures:

(a) The pilot's prime responsibility is to fly the aircraft and avoid hazards.Do not attempt to observe or assist the observer other than to ensurethat the aircraft is positioned correctly. Remember, the safety of theaircraft and its crew must never be put at risk for the sake of economyor to save time;

(b) The aircraft shall be manoeuvred in such a manner that a forced landingcan be carried out following a mechanical failure or loss of control, clearof structures and without danger to persons on the ground;

(c) Carry out early morning or late afternoon operations 'down sun' or waituntil the sun is in a more favourable position.

(d) Do not approach a powerline other than at a pole and not at a greaterangle to the line than 30 degrees.

....


© AEROSERVICE 2000



6.7 OPERATION

(1) All inspection flights shall be carried out in visual meteorological conditionsand the pilot in command must adhere to the following ... (Cont’d)

(e) Wherever possible, the powerlines being inspected should be kept onthe pilot's side of the aircraft.

(f) Where powerlines run parallel with a roadway, the aircraft shall bepositioned to the side of the line away from the road.

(g) Position the aircraft approximately 60 metres (200 feet) to one side and100 feet above the line to be inspected. Remember that distance froma single conductor is virtually impossible to judge by human eye and theflight path must therefore be regulated by reference to other visualfeatures.

(h) If visual contact with the conductor(s) is lost, immediately turn 90 degreesaway from the powerline and re-approach the line at a pole. Never lookback - if unsure reposition the aircraft for another inspection pass.

(i) When inspecting lengthy cable spans ensure that the increasing angleof the conductor, when combined with rising terrain, will not exceed themaximum climbing angle of the aircraft.

(j) Powerlines located on sharply rising terrain or traversing steep slopesshall be inspected on down hill runs and then only if the pilot incommand is able to establish that there is a satisfactory escape route forthe aircraft upon completion of the down hill run.

(k) If operating in mountainous areas beware of the sudden temporaryreduction in visibility when passing from sunlight to shade and vise-versa.

(l) In areas of flat terrain, the aircraft may be flown in the normal cruiseconfiguration but in every other circumstance, adopt the same techniqueas for flight in bad visibility and reduce airspeed to the lowest safe cruisespeed specified for that aircraft.

(2) It is emphasised that ultimately the sole authority for the safety of theoperation is the pilot in command who may cancel or terminate a sortie at anystage because of adverse weather or other factors affecting safety.

GG

RAC Operations Manual Part ABD.pdf - Redcliffe Aero Club

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Transcript of RAC Operations Manual Part ABD.pdf - Redcliffe Aero Club