LJ-904 N94HB Status Report - Sandhills Global

Standard Airworthiness Certificate Issued 04/04/1980

Hourmeter

4876.1

TRACK CODES HoursCycles Serial Number

AC 11,804.3

(ENGINE #'s listed below)

LE 11,689.0 PCE-24782

RE 11,687.9 PCE-24783

LP 122.4 TSO BUA20404

RP 14,556.8 TSO BUA21991

1. Enter "Hours" in Hours and Tenth format. Number will be rounded off. DO NOT USE MINUTES

2. Enter Calendar limits in number of months only. (ie. 4 years would be entered as 48)

Inspection Limits Last Action Remaining Time Next Compliance Due

Component Part Number / Remarks ATA TaskTrack

CodeAction Required

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(months)Hours Cycles Date Hours Cycles

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(months)Hours Cycles

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(Mo/Yr)Hours Cycles

TIME LIMITS / MAINT. CHECKS 5

Phase 1 inspection 5 INSP AC 24 297 2/13/20 11,660 12,853 7 153 Feb-22 11,957

Phase 2 inspection 5 INSP AC 497 2/13/20 11,660 12,853 353 12,157

Phase 3 inspection 5 INSP AC 600 2/4/21 11,757 12,949 553 12,357

Phase 4 inspection 5 INSP AC 24 800 2/4/21 11,757 12,949 18 753 Feb-23 12,557

OR Alternate Phase Inspection Program

Phase 1 and 2 Inspection 5 AWL AC Inspection 12 200

Phase 3 and 4 Inspection 5 AWL AC Inspection 24 400

OR Bienniel Inspection Program

Complete Inspection 5 AWL AC Inspection 24

Interim Inspection 5 AWL AC Inspection 12

ENGINES

Minor and Routine Periodic Inspections P&WC Maint. Manual 5 PWC AC Inspection 12 200 2/4/21 11,757 12,949 6 153 Feb-22 11,957

LEVELING & WEIGHING 8

Weigh Aircraft 8 AC Weigh 36 8/20/20 11,704 12,891 25 Aug-23

SERVICING 12

200 hour lubrication 12 AC Lube 200 2/4/21 11,757 12,949 153 11,957



1,200 hour lubrication 12 AC Lube 1,200 2/12/16 10,960 12,135 356 12,160

5 years or 1,200 hours rudder trim tab actuator

lubrication12 AC Lube 60 1,200 2/28/17 11,116 12,326 7 511 Feb-22 12,316

1000 cycle or 30 month lubrication 12 AC Lube 30 1,000 2/15/19 11,500 12,638 1 655 Aug-21 13,638

Wing bolt lube Annually 12 AC lube 12

AIRCONDITIONING 21

Air Condition motor brushes 1,000 Hours 21 SPL AC Inspect 1,000 2/20/18 11,295 12,495 512 13,495

Beech, Model C90 King Air, S/N LJ-904, N94HB12,683

144.5

Current Date

12,983

12,603

CENTRAL FLYING SERVICE 1501 Bond Street, Little Rock, Arkansas 72202

(501) 374-2150 1-800-888-5387 CRS# HBKR587E

29-Jul-2021

Missing or

Unconfirmed dataPast Due N/A

King Air® 90 Series MM Rev. D0 dated 1 December 2019 & ALM Reissue C (Feb 2016)

3. The "Track Code" is used to indicate which item is used to track component time. (example - A component installed on #1 engine will use the #1 engine time to

calculate "Accumulated Time" for that component. Enter the appropriate "Track Code" EXACTLY as listed in table at left.

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Cabin Altitude Warning Pressure Switch Test

(Ref. AMM ch. 21-30-11, 501)12 Months 21 SPL AC Test 12 2/4/21 11,757 12,949 6 Feb-22

Combustion heater overhaul (LJ-1 thru LJ-501)3,000 acft hrs or 1,500

heater hrs. (Ref Janitrol

Aero SB 55)

21 05-11-00 AC Overhaul 3,000

Combustion heater pressure test (LJ-1 thru LJ-

501)

1,000 acft hrs or 500

heater hrs. (Ref Janitrol

Aero SB 55)

21 SPL AC Test 500

Evaporator Air Filter(s) 12 05-11-00 AC Replace 400 2/4/21 11,757 12,949 353 12,157

Pneumatic flow control unit solenoid valve filter,

left

Replace filter P/N

1520161 every 600

hours

21 05-11-00 AC Replace 600


left (clean 800 hrs, replace as necessary)

Clean filter P/N

1520173 every 800

hours

21 05-11-00 AC Clean 800 2/28/17 11,116 12,326 111 11,916


right

Replace filter P/N

1520161 every 600

hours

21 05-11-00 AC Replace 600


right (clean every 800 hrs, replace as necessary)

Clean filter P/N

1520173 every 800

hours

21 05-11-00 AC Clean 800 2/28/17 11,116 12,326 111 11,916

Heater Ignition Vibrator (LJ-1 thru LJ-501) 2,000 hrs of operation 21 05-11-00 HTR Overhaul

Heater ignition Vibrator - Switch Points (LJ-1

thru LJ501)600 hrs of operation 21 05-11-00 HTR Switch 600

Pressurization control filter (LJ-572 thru LJ-574,

LJ-641 and After, LW-123 and After; and earlier

aircraft w/Beech Kit No. 100-4004-1)

Replace every 800 hours

of operation and clean

filter housing

21 05-11-00 AC Replace 800 2/13/20 11,660 12,853 656 12,460

Recirculation air filter (LJ-1 thru LJ-75) 12 05-11-00 AC Replace 400

Supercharger (LJ-1 thru LJ501) 2,400 hrs of operation 21 05-11-00 AC Overhaul 2,400

Supercharger gearbox (LJ-1 thru LJ501) 3,600 hrs of operation 21 05-11-00 AC Overhaul 3,600

Supercharger gearbox oil filter (LJ-1 thru LJ501) 200 hrs of operation 12 05-11-00 AC Replace 600

Supercharger Hydraulic Pump filter (LJ-1 thru

LJ-113 except LJ-76)

1st 200 hrs of operation

then each 600 hrs of

operation

12 05-11-00 AC Replace 600

AUTO FLIGHT 22

COMMUNICATIONS 23

CVR Underwater Locator Beacon (LJ-1353, LJ-

1354, LJ-1357 and After)

Functional test unit and

batteries for proper

operation every 24

months.

23 ALM AC Test 24

CVR Underwater Locator Beacon batteries (LJ-

1353, LJ-1354, LJ-1357 and After)

Replace batteries every 6

years.23 ALM AC Replace 72

ELECTRICAL POWER 24

Starter-Generator, left engine (Check bus

voltage on outbound run)1,000 hrs 24 05-11-00 AC Overhaul 1,000 2/15/19 11,500 12,638 696 12,500

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Starter-Generator, right engine (Check bus

voltage on outbound run)1,000 hrs 24 05-11-00 AC Overhaul 1,000 2/13/20 11,660 12,853 856 12,660

Standby Power Supply Battery (PS835) annual

capacity test

L-3 Avionics Systems

CMM24 CMM AC Test 12

Standby Power Supply Battery (PS835) 6 month

periodic check and load test

L-3 Avionics Systems

CMM24 SPL AC Test 6

EQUIPMENT AND FURNISHINGS 25

ELT battery 25 05-11-00 AC Replace 72 12/29/16 11,098 12,306 17 Dec-22

FAR 91.207(d) ELT test 25 FAR AC Test 12 2/4/21 11,757 12,949 6 Feb-22

FIRE PROTECTION 26

Fire Extinguisher Hydrostatic Test, Cabin 26 ALM AC Test 144 2/28/17 11,116 12,326 91 Feb-29

Fire extinguisher 6-year maintenanance, cabin 26 NFPA AC Inspect 72 2/28/17 11,116 12,326 19 Feb-23

Fire extinguisher weight check, cabin 26 NFPA AC Weigh 12 2/4/21 11,757 12,949 6 Feb-22

Fire Extinguisher Hydrostatic Test, Flight

Compartment26 SPL AC Test 144 2/28/17 11,116 12,326 91 Feb-29

Fire extinguisher 6-year maintenanance, cockpit 26 NFPA AC Inspect 72 2/28/17 11,116 12,326 19 Feb-23

Fire extinguisher weight check, cockpit 26 NFPA AC Weigh 12 2/4/21 11,757 12,949 6 Feb-22

Engine Fire Extinguisher Bottle Hydrostatic

Test, Left Engine

Hydrostatically test

bottle every 5 years26 ALM AC Test 60

Fire extinguisher squib, left engine life limit 6 Years 26 ALM AC Replace 48

Fire extinguisher squib, left engine install limit 4 Years 26 ALM AC Replace 72

Engine Fire Extinguisher Bottle Hydrostatic

Test, Right Engine


bottle every 5 years26 ALM AC Test 60

Fire extinguisher squib, right engine life limit 6 Years 26 ALM AC Replace 48

Fire extinguisher squib, right engine install limit 4 Years 26 ALM AC Replace 72

FLIGHT CONTROLS 27

Ailerons, Detailed Inspection3,600 Hours Initial/ 800

Hours Subsequent27 SPL AC Inspect 800 2/13/20 11,660 12,853 656 12,460

Flexible Shafts, Flaps (LJ-1 thru LJ-526 without

Kit 99-4017-1 S)27 SPL AC Inspect 2,000

Flexible Shafts, Flaps (LW-1 and after, LJ-527

and after, and earlier airplanes with Kit 99-4017-

1 S)

27 SPL AC Inspect 5,000 2/27/08 8,988 9,884 1,901 14,884

Flight control pulley brackets and castings 10,000 cyc / 5,000 cyc 27 SPL AC Inspect 5,000 2/27/08 8,988 9,884 1,901 14,884

FLAPS - Remove flaps and inspect flap attach

brackets, flap structure, tracks, and attachment

hardware for wear. Replace all roller bearings

with new. (Special Inspection 55)

3,000 CYCLES OR

THREE YEARS 27 SPL AC Inspect 36 3,000 2/13/20 11,660 12,853 19 2,870 Feb-23 15,853

FUEL 28

HYDRAULIC POWER 29

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LANDING GEAR 32

Axle assembly and torque knee, left MLG 32 SPL AC Inspect 72 8,000 9/12/19 11,548 12,727 49 7,744 Sep-25 20,727

Axle assembly and torque knee, NLG 32 SPL AC Inspect 72 8,000 9/12/19 11,548 12,727 49 7,744 Sep-25 20,727

Axle assembly and torque knee, right MLG 32 SPL AC Inspect 72 8,000 9/12/19 11,548 12,727 49 7,744 Sep-25 20,727

Brake system hoses, left (Only hoses exposed in

wheel well)60 mos 32 05-11-00 AC Replace 60 2/20/18 11,295 12,495 19 Feb-23

Brake system hoses, right (Only hoses exposed

in wheel well)60 mos 32 05-11-00 AC Replace 60 2/20/18 11,295 12,495 19 Feb-23

Drag brace assembly, left MLG 32 SPL AC Inspect 72 8,000 9/12/19 11,548 12,727 49 7,744 Sep-25 20,727

Drag brace assembly, NLG 32 SPL AC Inspect 72 8,000 9/12/19 11,548 12,727 49 7,744 Sep-25 20,727

Drag brace assembly, right MLG 32 SPL AC Inspect 72 8,000 9/12/19 11,548 12,727 49 7,744 Sep-25 20,727

Landing gear actuator clevis, left (LJ-1 thru LJ-

1062; LW-1 & after) - Inspect clevis hole for

wear (Disassembly required). (Ref. Component

Maintenance Manual, 32-00-00).

32 SPL AC Inspect 1,000 5/23/19 11,530 12,712 729 13,712

Landing gear actuator clevis, nose (LJ-1 thru LJ-


excessive wear (Disassembly required) (Ref.

Component Maintenance Manual, 32-00-00).

32 SPL AC Inspect 1,000 5/23/19 11,530 12,712 729 13,712

Landing gear actuator clevis, right (LJ-1 thru LJ-


wear (Disassembly required). (Ref. Component

Maintenance Manual, 32-00-00).

32 SPL AC Inspect 1,000 5/23/19 11,530 12,712 729 13,712

Landing gear actuator, left (mechanical) 32 05-11-00 AC Overhaul 72 8,000 5/23/19 11,530 12,712 46 7,729 May-25 20,712

Landing gear actuator, left (mechanical) End-Play Check 32 SPL AC Inspect 30 1,000 5/23/19 11,530 12,712 4 729 Nov-21 13,712

Landing gear actuator, left (mechanical) Lubrication 32 SPL AC Lubricate 30 1,000 5/23/19 11,530 12,712 4 729 Nov-21 13,712

Landing gear actuator, nose (mechanical) 32 05-11-00 AC Overhaul 72 8,000 5/23/19 11,530 12,712 46 7,729 May-25 20,712

Landing gear actuator, nose (mechanical) End-Play Check 32 SPL AC Inspect 30 1,000 5/23/19 11,530 12,712 4 729 Nov-21 13,712

Landing gear actuator, nose (mechanical) Lubrication 32 SPL AC Lubricate 30 1,000 5/23/19 11,530 12,712 4 729 Nov-21 13,712

Landing gear actuator, right (mechanical) 32 05-11-00 AC Overhaul 72 8,000 5/23/19 11,530 12,712 46 7,729 May-25 20,712

Landing gear actuator, right (mechanical) End-Play Check 32 SPL AC Inspect 30 1,000 5/23/19 11,530 12,712 4 729 Nov-21 13,712

Landing gear actuator, right (mechanical) Lubrication 32 SPL AC Lubricate 30 1,000 5/23/19 11,530 12,712 4 729 Nov-21 13,712

Landing gear hydraulic system filter and packing

At 1st 200-hour

inspectection then every

1,200 hours or 1,000

cycles

32 05-11-00 AC Replace 1,200 1,000

Landing gear motor (mechanical) 8,000 Cycles or 6 Years 32 05-11-00 AC Overhaul 72 8,000 2/28/17 11,116 12,326 19 7,343 Feb-23 20,326

Landing gear retraction and extension teflon

hydraulic hoses120 mos 32 05-11-00 AC Replace 120

Main gear wheel assembly, Left CMM 32 SPL AC Inspect

Main gear wheel assembly, Right CMM 32 SPL AC Inspect

Nose wheel assemblyCleveland Nose Wheel

p/n 40-20432 AC Inspect 12

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Retract Gearbox and Clutch (mechanical gear) 8,000 Cycles or 6 Years 32 SPL AC Inspect 72 8,000 2/28/17 11,116 12,326 19 7,343 Feb-23 20,326

Shock absorber assembly, left MLG 32 SPL AC Inspect 72 8,000 9/12/19 11,548 12,727 49 7,744 Sep-25 20,727

Shock absorber assembly, NLG 32 SPL AC Inspect 72 8,000 9/12/19 11,548 12,727 49 7,744 Sep-25 20,727

Shock absorber assembly, right MLG 32 SPL AC Inspect 72 8,000 9/12/19 11,548 12,727 49 7,744 Sep-25 20,727

Trunnion bolt holes and drag brace attach holes,

left MLG8,000 Cycles or 6 Years 32 SPL AC Inspect 72 8,000 9/12/19 11,548 12,727 49 7,744 Sep-25 20,727


NLG8,000 Cycles or 6 Years 32 SPL AC Inspect 72 8,000 9/12/19 11,548 12,727 49 7,744 Sep-25 20,727


right MLG8,000 Cycles or 6 Years 32 SPL AC Inspect 72 8,000 9/12/19 11,548 12,727 49 7,744 Sep-25 20,727

LIGHTS 33

Edge lighted panel assemblies 2,000 hours or 4 years 33 SPL AC Inspect 48 2,000 2/15/19 11,500 12,638 19 1,696 Feb-23 13,500

Pilots fuel control panel and lower edglighted

panel, Copilot's edgelighted circuit breaker

panel, and Wiring circuitry below the storm

windows. (Panel removal is required.)

12 Months 33 SPL AC Inspect 12 2/13/20 11,660 12,853 (5) Feb-21

NAVIGATION 34

ADC No. 1 - FAR 91.411 check 34 SPL AC Test 24

ADC No. 2 - FAR 91.411 check 34 SPL AC Test 24

Altimeter No. 1 - FAR 91.411 check 34 SPL AC Test 24 7/22/20 12 Jul-22

Altimeter No. 2 - FAR 91.411 check 34 SPL AC Test 24 10/11/19 2 Oct-21

Altimeter, Standby - FAR 91.411 check 34 SPL AC Test 24

Static Pressure System - FAR 91.411 check 34 SPL AC Test 24 10/11/19 2 Oct-21

Transponder No. 1 - FAR 91.413 check 34 FAR AC Test 24 11/27/19 4 Nov-21

Transponder No. 2 - FAR 91.413 check 34 FAR AC Test 24

OXYGEN 35

Oxygen cylinder (lightweight composite)

Cylinder service life not

to exceed 15 years or

10,000-fill and depletion

cycles, whichever comes

first

35 ALM AC Replace 180

Oxygen cylinder (lightweight composite)

Inspect and

Hydrostatically Test

Every 5 Years.

Overhaul regulator

when oxygen cylinder

is hydrostatically

tested.

35 ALM AC Hydrostatic Test 60

Oxygen Cylinder (Standard weight) DOT 3AA

49CFR 173.34


every 5 years (DOT

Regulation). Service life

unlimited.

35 ALM AC Hydrostatic Test 60 4/25/19 11,530 12,712 33 Apr-24

Oxygen Cylinder (Lightweight) DOT 3HT 1850

49CFR 173.34

Replace after 24 years or

4,380 refills.35 ALM AC Replace 288

Oxygen Cylinder (lightweight) DOT 3HT 1850

49CFR 173.34


every 3 years (DOT

Regulation).

35 ALM AC Test 36

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PNEUMATIC 36

Pneumatic system hose couplings (LJ6 thru LJ-

716, LW-1 thru LW-223)

Replace the two

106200H hose couplings

every 5 years

36 05-11-00 AC Replace 60

VACUUM 37

Instrument air filter (LJ-1 thru LJ-1846, LJ-1848

thru LJ-185237 05-11-00 AC Replace 800 2/20/18 11,295 12,495 291 12,095

STRUCTURES 51

Skin, Exterior Airframe 10,000 cyc / 1,000 cyc 51 SPL AC Inspect 1,000 2/4/21 11,757 12,949 966 13,949

DOORS 52

Cabin Entrance Door Forward and Aft Side

Latches or Bayonets52 ALM AC Replace 5,000 9/9/08 9,160 10,085 2,102 15,085

Upper Door Hook Mechanism (Includes the pins,

bracket, spring, arm and hooks)52 ALM AC Replace 10,000 2/27/08 8,988 9,884 6,901 19,884

FUSELAGE 53

Fuselage Inspection (4.6 PSI cabins), (LJ-1 thru

LJ-985, LJ-987 thru LJ-995, LJ-997 thru LJ-

1010, LW-1 and After)

9,000 cyc / 3,000 cyc 53 SPL AC Inspect 3,000 9/12/19 11,548 12,727 2,744 15,727

Fuselage Inspection (5.0 PSI cabins), (LJ-986,

LJ-996, LJ-1011 and after)6,000 cyc / 3,000 cyc 53 SPL AC Inspect 6,000

STABILIZERS 55

Horizontal Stabilizer (Elevator) Structural

Inspection Procedure10,000 hrs / 5,000 hrs 56 SPL AC Inspect 5,000 2/20/18 11,295 12,495 4,491 16,295

Vertical Stabilizer (Rudder) Structural Inspection

Procedure10,000 hrs / 5,000 hrs 56 SPL AC Inspect 5,000 2/20/18 11,295 12,495 4,491 16,295

WINDOWS 56

Windshield attach screws, left 56 ALM AC Replace 10,000 9/13/17 11,189 12,412 9,429 22,412

Windshield attach screws, right 56 ALM AC Replace 10,000 2/16/09 9,309 10,272 7,289 20,272

WINGS 57

All wing attach fitting flat surfaces, depressions,

counterbores and bolt bores (LJ-1 Thru LJ-1084,

LJ-1086, LJ-1087; LW-1 Thru LW-347 without

Spar Kit 90-4077-1)

1,000 hrs or 3 yrs,

whichever occurs first57 SIRM AC Inspect 36 1,000 9/12/19 11,548 12,727 13 744 Sep-22 12,548

All wing attach fitting flat surfaces, depressions,

counterbores, bolt bores and the radii at the

bottom of the fittings which house the barrel nuts

(LJ-1 Thru LJ-1084, LJ-1086, LJ-1087; LW-1

Thru LW-347 with Spar Kit 90-4077-1)

1,000 hrs or 3 yrs,

whichever occurs first57 SIRM AC Inspect 36 1,000

Area under center section floor board between

the forward and aft spars (LJ-1 Thru LJ-1084, LJ-

1086, LJ-1087; LW-1 Thru LW-347)

1,000 hrs or 3 yrs,


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Four fastener holes in the lower forward spar cap

at the wing root (LJ-1 Thru LJ-1084, LJ-1086,

LJ-1087; LW-1 Thru LW-347 without Spar Kit

90-4077-1)

1,000 hrs or 3 yrs,


Lower Forward Wing Bolt and Nut (LJ-1 thru LJ-

1084, LJ-1086 and LJ-1087)

Replace at 20 years of

service or 20,000 hours

whichever occurs first

57 ALM AC Replace 240 20,000 8/28/13 10,461 11,630 145 18,657 Aug-33 30,461

Lower Forward Wing Bolt and Nut (LW-1 thru

LW-347 without Spar Kit 90-4077-1)




57 SIRM AC Replace 180 15,000

Lower forward wing fitting-to-spar attachment

(LJ-1 Thru LJ-1084, LJ-1086, LJ-1087; LW-1

Thru LW-347 without Spar Kit 90-4077-1)

1,000 hrs or 3 yrs,


Lower surface of lower forward spar cap from

nacelle to fueslage (LJ-1 Thru LJ-1084, LJ-1086,

LJ-1087; LW-1 Thru LW-347 without Spar Kit

90-4077-1)

1,000 hrs or 3 yrs,


Nacelle splice plates (see 57-13-04) 57 ALM AC Replace 20,000 0 8,196 20,000

Nacelle splice plates (see 57-13-04) 10,000/1,000 hrs 57 SIRM AC Inspect 1,000 2/12/16 10,960 12,135 156 11,960

NACELLE SPLICE PLATES - Inspect the splice

plates for condition and corrosion (Special

Inspection 56)

10,000 HOURS

INITIAL/ 1,000

HOURS RECURRING

57 SPL AC Inspect 1,000 2/13/20 11,660 12,853 856 12,660

Outboard wing lower main spar cap from wing

attach fitting to tie down lug (LJ-1 Thru LJ-

1084, LJ-1086, LJ-1087; LW-1 Thru LW-347)

1,000 hrs or 3 yrs,


Outboard wing panel upper and lower main spar

caps (left & right)5 yr / 1 yr 57 SPL AC Inspect 12 2/4/21 11,757 12,949 6 Feb-22

Spar cap in nacelle, inboard of wheel well (LJ-1

Thru LJ-1084, LJ-1086, LJ-1087; LW-1 Thru

LW-347 without Spar Kit 90-4077-1)

1,000 hrs or 3 yrs,


Spar cap in wheel well (LJ-1 Thru LJ-1084, LJ-

1086, LJ-1087; LW-1 Thru LW-347 without

Spar Kit 90-4077-1)

1,000 hrs or 3 yrs,


Lower Aft Wing Bolts and Nuts (LJ-1 and After;

LW-1 and After)





Upper Aft Wing Bolts and Nuts (LJ-1 and After;

LW-1 and After)





Upper Forward Wing Bolts and Nuts (LJ-1 and

After; LW-1 and After)





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Wing Attachment Bolts and Nuts (LW-1 thru

LW-347; LJ-1 thru LJ-1087, except LJ-1085

without Spar Kit No. 90-4077-1

1,000 HOURS OR 3

YEARS57 SIRM AC Inspect 36 1,000 9/12/19 11,548 12,727 13 744 Sep-22 12,548

Wing bolts torque Ref. SIRM 57 SIRM AC Check 2/13/20 11,660 12,853

PROPELLERS 61

Propeller Overhaul, Left Ref. mfr. SB/SL 61 05-11-00 LP Overhaul 60 3,000 5/5/20 0 45 2,878 May-25 3,000

Propeller Overhaul, Right Ref. mfr. SB/SL 61 05-11-00 RP Overhaul 60 3,000 2/13/20 14,412 43 2,856 Feb-25 17,412

Propeller Periodic Inspection, Left P.O.M. No. 139 61 LP Inspect 12 400 2/4/21 6 Feb-22

Propeller Periodic Inspection, Right P.O.M. No. 139 61 RP Inspect 12 400 2/4/21 14,510 6 353 Feb-22 14,910

Overspeed Governor, LeftUnit installed with 191.8

hrs61 05-11-00 AC Overhaul 6,308 8/24/10 9,741 10,837 4,245 16,049

Overspeed Governor, RightUnit installed with 261.5

hrs61 05-11-00 AC Overhaul 6,239 8/24/10 9,741 10,837 4,175 15,979

Propeller Governor, Left8210-002AE, s/n

199245861 05-11-00 LE Overhaul 3,600 1/30/06 8,106 8,734 17 11,706

Propeller Governor, Right8210-002AE, s/n

199586261 05-11-00 RE Overhaul 3,600 11/16/05 8,060 8,711 (28) 11,660

POWERPLANT 71

Engine Mount Vibration Isolators (Left) Inspect

vibration isolators for deterioration, damage and

attachment (Ref. CMM, 71-00-00)

Engine TBO or 4,000

Hours71 SPL AC Inspect 4,000 5/17/04 7,603 8,248 (201) 11,603

Engine Mount Vibration Isolators (Right) Inspect

vibration isolators for deterioration, damage and

attachment (Ref. CMM, 71-00-00)

Engine TBO or 4,000

Hours71 SPL AC Inspect 4,000 5/17/04 7,603 8,248 (201) 11,603

Engine #1 deceleration check (For post SB1568 -

21 and -28 engines) Not required for FCU identified

with "RE52", "SB 73-3" or with a serial number that

contains the letter F as a prefix

P&W M.M. 71 P&WC LE Check 400

Engine #2 deceleration check (For post SB1568 -

21 and -28 engines) Not required for FCU identified

with "RE52", "SB 73-3" or with a serial number that

contains the letter F as a prefix

P&W M.M. 71 P&WC RE Check 400

ENGINE 72

1st P.T. disc, left engine 3022412, s/n 3D999 71 AW Lmt LE Replace 20,000 4/4/80 0 0 7,397 20,000

1st P.T. disc, right engine 3022412, s/n 6D789 71 AW Lmt RE Replace 20,000 4/4/80 0 0 7,317 20,000

2nd stage, left engine 3013712, s/n A6209 71 AW Lmt LE Replace 17,152 3/10/94 3,617 3,634 8,183 20,786

2nd stage, right engine 3013712, s/n 3B760 71 AW Lmt RE Replace 20,181 11/16/05 8,060 8,711 16,209 28,892

3rd stage, left engine 3011713, s/n 5D096 71 AW Lmt LE Replace 25,000 4/4/80 0 0 12,397 25,000

3rd stage, right engine 3011713, s/n 4H638 71 AW Lmt RE Replace 21,181 11/16/05 8,060 8,711 17,209 29,892

CT Disc, Left engine 3013411, s/n 5D639 71 AW Lmt LE Replace 16,000 4/4/80 0 0 3,397 16,000

CT Disc, right engine 3013411, s/n 5D598 71 AW Lmt RE Replace 16,000 4/4/80 0 0 3,317 16,000

Impeller, left engine 3013176, s/n 7A653 71 AW Lmt LE Replace 19,000 4/4/80 0 0 6,397 19,000

Impeller, right engine 3013176, s/n 7A555 71 AW Lmt RE Replace 19,000 4/4/80 0 0 6,317 19,000

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Rear hub, left engine 3013111, s/n 8D499 71 AW Lmt LE Replace 19,000 4/4/80 0 0 6,397 19,000

Rear hub, right engine 3013111, s/n A1333 71 AW Lmt RE Replace 15,125 4/4/80 0 0 2,442 15,125

Compressor wash, left engine 72 LE Wash 200 2/13/20 11,545 12,534 56 11,745

Compressor wash, right engine 72 RE Wash 200 2/13/20 11,543 12,574 56 11,743

Engine #1 Hot Section Borescope Inspection P&W M.M. 71 LE Inspect 400 2/15/19 11,385 12,375 96 11,785

Engine #2 Hot Section Borescope Inspection P&W M.M. RE Inspect 400 2/15/19 11,384 12,415 96 11,784

Engine Overhaul, left (SB1803-R6) 3,600 hrs 71 LE Overhaul 4,000 1/30/06 8,106 8,734 417 12,106

Engine Overhaul, right (SB1803 R6) 3,600 hrs 71 RE Overhaul 4,000 11/16/05 8,060 8,711 372 12,060

Fuel topping governor, left engine 71 LE Overhaul

Fuel topping governor, right engine 71 RE Overhaul

Hot Section Inspection, left engine SB 1803 R6 71 SPL LE Inspect 1,800 9/1/11 9,879 10,832 (10) 11,679

Hot Section Inspection, right engine SB 1803 R6 71 SPL RE Inspect 1,800 9/1/11 9,878 10,866 (10) 11,678

ENGINE FUEL & CONTROL 73

FCU overhaul, left engine 73 P&WC LE Overhaul 4,100 1/30/06 8,106 8,734 517 12,206

FCU overhaul, right engine 73 P&WC RE Overhaul 4,100 11/16/05 8,060 8,711 472 12,160

FCU drive body inspection/driveshaft bearing

replacement, left engineRemoval required 73 P&WC LE Inspect 3,600 1/30/06 8,106 8,734 17 11,706

FCU drive body inspection/driveshaft bearing

replacement, right engineRemoval required 73 P&WC RE Inspect 3,600 11/16/05 8,060 8,711 (28) 11,660

Flow Divider/Starting Control Installation

overhaul, left engineP&WC SB 1803 73 P&WC LE Overhaul 4,100 1/30/06 8,106 8,734 517 12,206

Flow Divider/Starting Control Installation

overhaul, right engineP&WC SB 1803 73 P&WC RE Overhaul 4,100 11/16/05 8,060 8,711 472 12,160

Fuel Heater overhaul, left engine P&WC SB 1803 73 P&WC LE Overhaul 4,100 1/30/06 8,106 8,734 517 12,206

Fuel Heater overhaul, right engine P&WC SB 1803 73 P&WC RE Overhaul 4,100 11/16/05 8,060 8,711 472 12,160

Fuel manifold adapter and nozzle assemblies,

Left engine73 LE Clean 400 2/15/19 11,385 12,375 96 11,785

Fuel manifold adapter and nozzle assemblies,

Right engine73 RE Clean 400 2/15/19 11,384 12,415 96 11,784

Fuel pump coupling In-Situ inspection (If

Sundstrand fuel pump installed), left engine

Included on Complete,

Phase 2 and Phase 473 Rec LE Inspect 600 2/15/19 11,385 12,375 296 11,985

Fuel pump coupling In-Situ inspection (If

Sundstrand fuel pump installed), right engine

Included on Complete,

Phase 2 and Phase 473 Rec RE Inspect 600

Fuel pump drive coupling and cover (AGB side)

inspection (If Sundstrand fuel pump installed),

left engine

Removal required 73 P&W LE Inspect 1,800 3/15/11 9,787 10,739 (102) 11,587

Fuel pump drive coupling and cover (AGB side)

inspection (If Sundstrand fuel pump installed),

right engine

Removal required 73 P&W RE Inspect 1,800

Fuel Pump overhaul, left engine (Argo-Tech

only)73 P&WC LE Overhaul 4,100

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Fuel Pump overhaul, right engine (Argo-Tech

only)73 P&WC RE Overhaul 4,100 11/16/05 8,060 8,711 472 12,160

Fuel Pump overhaul, left engine (Hamilton

Sundstrand)73 P&WC LE Overhaul 3,600 1/25/13 10,258 11,231 2,169 13,858

Fuel Pump overhaul, right engine (Hamilton

Sundstrand)73 P&WC RE Overhaul 3,600

Engine #1 Fuel Pump Inlet Screen P&W M.M. 73 P&WC LE Check 600 2/4/21 11,642 12,569 553 12,242

Engine #2 Fuel Pump Inlet Screen P&W M.M. 73 P&WC RE Check 600 2/4/21 11,641 12,649 553 12,241

Engine #1 Fuel Pump Outlet Filter P&W M.M. 73 P&WC LE Replace 600 2/4/21 11,642 12,569 553 12,242

Engine #2 Fuel Pump Outlet Filter P&W M.M. 73 P&WC RE Replace 600 2/4/21 11,641 12,649 553 12,241

P3 Filter, left engine (LJ-1727, LJ-1754, LJ-

1756 and After)

Replace at 1,000 hours.

Refer to applicable

engine maintenance

manual.

73 LE Replace 1,000

P3 Filter, right engine (LJ-1727, LJ-1754, LJ-

1756 and After)

Replace at 1,000 hours.

Refer to applicable

engine maintenance

manual.

73 RE Replace 1,000

P3 filter drain valve housing assembly, left

engine (Post SB 1495 (-135A) engines only)

Refer to Engine

Maintenance Manual for

procedure

73 P&WC LE Clean/Inspect 200

P3 filter drain valve housing assembly, right

engine (Post SB 1495 (-135A) engines only)

Refer to Engine

Maintenance Manual for

procedure

73 RE Clean/Inspect 200

IGNITION 74

Ignition Exciter overhaul, left engine P&WC SB 1803 74 P&WC LE Overhaul 4,100 1/30/06 8,106 8,734 517 12,206

Ignition Exciter overhaul, right engine P&WC SB 1803 74 P&WC RE Overhaul 4,100 11/16/05 8,060 8,711 472 12,160

Ignition Exciter inspection, Engine #1 P&W M.M. 74 P&WC LE Inspect 400 2/4/21 11,642 12,569 353 12,042

Ignition Exciter inspection, Engine #2 P&W M.M. 74 P&WC RE Inspect 400 2/4/21 11,641 12,649 353 12,041

Ignition Cables inspection, Engine #1 P&W M.M. 74 P&WC LE Inspect 400 2/4/21 11,642 12,569 353 12,042

Ignition Cables inspection, Engine #2 P&W M.M. 74 P&WC RE Inspect 400 2/4/21 11,641 12,649 353 12,041

Spark Igniters inspection, Engine #1 P&W M.M. 74 P&WC LE Inspect 400 2/4/21 11,642 12,569 353 12,042

Spark Igniters inspection, Engine #2 P&W M.M. 74 P&WC RE Inspect 400 2/4/21 11,641 12,649 353 12,041

AIR 75

Compressor Bleed Valve overhaul, left engine P&WC SB 1803 75 P&WC LE Overhaul 4,100 9/1/11 9,879 10,832 2,290 13,979

Compressor Bleed Valve overhaul, right engine P&WC SB 1803 75 P&WC RE Overhaul 4,100 10/19/11 9,920 10,914 2,332 14,020

Compressor Bleed Valve inspection (in

conjuction w/HSI), left engineP&W M.M. 75 P&WC LE Inspect 1,800 9/1/11 9,879 10,832 (10) 11,679

Compressor Bleed Valve inspection (in

conjuction w/HSI), right engineP&W M.M. 75 P&WC RE Inspect 1,800 10/19/11 9,920 10,914 32 11,720

ENGINE CONTROLS 76

Power Lever Detent Pin 76 SPL AC Inspect 1,200 2/20/18 11,295 12,495 691 12,495

OIL 79

Engine oil change, left Exxon 2380 79 LE Info 1/30/06 8,106 8,734

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Engine oil change, right Exxon 2380 79 RE Info 11/16/05 8,060 8,711

Engine oil filter, left 79 SPL LE Replace 1,000 2/4/21 11,642 12,569 953 12,642

Engine oil filter, right 79 SPL RE Replace 1,000 2/4/21 11,641 12,649 953 12,641

Magnetic chip detector, left engine Acft w/o kit 100-9013-1 79 SPL LE Inspect 25

Magnetic chip detector, right engine Acft w/o kit 100-9013-1 79 SPL RE Inspect 25

Magnetic chip detector contact bridge test, left

engineP&W M.M. 79 LE Check 12 600 2/4/21 11,642 12,569 6 553 Feb-22 12,242

Magnetic chip detector contact bridge test, right

engineP&W M.M. 79 RE Check 12 600 2/4/21 11,641 12,649 6 553 Feb-22 12,241

Magnetic chip detector continuity check, left

engineP&W M.M. 79 LE Check 200 2/4/21 11,642 12,569 153 11,842

Magnetic chip detector continuity check, right

engineP&W M.M. 79 RE Check 200 2/4/21 11,641 12,649 153 11,841

AGB scavenge oil pump inlet screen, left engine 79 P&W LE Inspect 1,000 2/12/16 10,845 11,814 156 11,845

AGB scavenge oil pump inlet screen, right

engine79 P&W RE Inspect 1,000 2/12/16 10,844 11,845 156 11,844

SOAP check, left engine oil 79 LE Check 200 2/4/21 11,642 12,569 153 11,842

SOAP check, right engine oil 79 RE Check 200 2/4/21 11,641 12,649 153 11,841

ON CONDITION 98

Special Use Aircraft limitations research 98 AWL

ICA INSPECTIONS 99

Avidesign 3 year wing strap inspection 99 AC Inspect 36

Cleveland main gear wheel assembly, Left 32 ICA AC Inspect

Cleveland main gear wheel assembly, Right 32 ICA AC Inspect

Cleveland nose wheel assembly Due @ Tire Change 32 ICA AC Inspect

Concorde Battery Inspection 24 ICA AC Inspection 6 200

Concorde Battery Inspection 24 ICA AC Inspection 12 200

Concorde Battery Inspection (Concorde ICA)12 mos or 600 hrs then

each 3 mos or 200 hrs24 ICA AC Inspection 3 200

Teledyne Gill Valve-Regulated Lead-Acid

Aircraft Battery (Ref. Teledyne Battery Products

Document Number Q01-1100)

800 hrs or 11 mos then

each 400 hrs or 6 mos24 ICA AC

Inspect / Cap

check6 400

Teledyne Gill 7000 Series LT Valve-Regulated

Lead-Acid Battery (Ref. Teledyne Battery Products

Document Number TD14-8-01)

1,800 hrs or 18 mos then

each 900 hrs or 9 mos24 ICA AC

Inspect / Cap

check9 900 2/4/21 11,757 12,949 3 853 Nov-21 12,657

Raisbeck/Beechcraft enhanced performance

leading edge inspection99 AC Inspect 200

Raisebeck/Beechcraft Quiet Turbo-fan Propeller

installation99 AC Inspect 200

Raisebeck/Beechcraft Ram Air recovery system 99 AC Inspect 200

RDR 2000 - ICA requirement 99 AC Inspect

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SAFT Nicad battery capacity test 24 AC Test 200

SKY497 - ICA 99 AC Inspect

WX500 Stormscope - ICA 99 AC Inspect

74-16-04 (08/06/1974) Restricted Elevator

TravelN/A Acft S/N AD FAR AC

74-24-03 (11/22/1974) Strobe Light System N/A Acft S/N AD FAR AC

76-04-02 (02/26/1976) Seat Locking Pins N/A Acft S/N AD FAR AC

76-10-10 (05/28/1976) Cabin Door N/A Acft S/N AD FAR AC

76-22-02 (06/02/1977) 'Y' Type Shoulder

HarnessN/A Acft S/N AD FAR AC

77-02-04 (03/03/1977) Wing Tip Strobe Lights N/A Acft S/N AD FAR AC

77-07-06 (04/11/1977) Rudder Control Cable N/A Acft S/N AD FAR AC

77-18-04 (09/12/1977) Cabin Pressurization N/A Acft S/N AD FAR AC

77-22-01 (08/23/1978) Fuselage Structure N/A Acft S/N AD FAR AC

78-05-06 (06/30/1978) Goodyear Flexible Fuel

CellsC/W at production AD FAR AC

78-11-06 (06/08/1978) Elevator Control Cable N/A Acft S/N AD FAR AC

78-22-05 (11/06/1978) Elevator Control Push

RodsN/A Acft S/N AD FAR AC

79-01-01 (01/08/1979) Screws in Control

SystemN/A Acft S/N AD FAR AC

80-09-03 R1 (06/11/1980) Placard -Oxygen N/A Acft S/N AD FAR AC

81-09-01 (04/23/1981) Landing Gear Retract

SystemAD FAR AC 7/1/81 588

81-23-01 R1 (01/04/1982) Beech Kit or

Supplemental Type CertificateAD FAR AC 11/6/81 746

85-01-01 (02/06/1985) Acrylic Windows AD FAR AC

85-22-05 (11/12/1985) Nuts and Bolts

ReplacementN/A AD FAR AC 8/2/02 7,009 7,524

87-04-24 (04/14/1987) Elevator Trim Cable

SystemP/C/W AD FAR AC 8/2/02 7,009 7,524

87-22-01 R1 (09/30/1989) Nose landing gear

forkNew style fork installed AD FAR AC Inspect 5/31/90 2,891

88-04-07 (04/18/1988) Wing Spar Nuts

InspectionSB 2248 Part II AD FAR AC 3/16/88 2,293

89-22-14 (11/17/1989) Aileron Flutter C/W par. (b) AD FAR AC 8/2/02 7,009 7,524

AIRWORTHINESS DIRECTIVES as of 02/02/2021 (Biweekly 2021-02)

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89-25-10 (01/04/1990) Wing Main Spar

InspectionSIRM AD FAR AC Inspect 1,000 9/12/19 11,548 12,727 744 12,548

90-08-17 (05/07/1990) Fuselage Moisture

Drain SystemAD FAR AC 5/31/90 2,891

92-07-05 (04/30/1992) Rudder trim tab SB 2365 P/C/W AD FAR AC 8/2/02 7,009 7,524

92-15-01 (08/21/1992) Truss-To-Firewall Bolts AD FAR AC 8/28/92 3,334

93-17-01 (10/12/1993) Leading Edge Fuel Cell

NipplesSB 2475 P/C/W AD FAR AC 4/22/94 3,708 3,748

97-06-06 (05/09/1997) Pilot and Copilot Chairs

Locking PinsAD FAR AC 5/14/97 4,889 5,095

97-23-17 (12/29/1997) Pneumatic Tubing AD FAR AC 2/12/98 5,236 5,535

97-25-01 (01/11/1998) Outflow/Safety Valve N/A valves S/Ns AD FAR AC 2/12/98 5,236 5,535

97-25-03 (01/21/1998) AFM - Limitations -

Power LeversAD FAR AC 2/12/98 5,236 5,535

98-04-24 (03/13/1998) AFM - Limitations

Section - Icing

C/W par. (a)(1) and

(a)(2)AD FAR AC 8/2/02 7,009 7,524

98-15-13 (08/28/1998) Rubber fuel hose AD FAR AC 5/5/99 5,805 6,176

98-25-02 (12/22/1998) SKYWATCH SKY497

Top-mounted AntennaNot installed AD FAR AC

99-10-07 (06/08/1999) Elevator Control Cable AD FAR AC 5/10/99 5,805 6,176

2000-02-15 (02/18/2000) Engine and Propeller

ConfigurationAD FAR AC 3/13/00 6,224 6,596

2001-23-17 (12/28/2001) Garmin GNS 430

unitsAD FAR AC 1/24/12 10,091 11,227

2002-01-10 (02/22/2002) Main Landing Gear

Torque KneesSB 32-3116 P/C/W AD FAR AC 8/2/02 7,009 7,524

2003-02-03 (03/07/2003) Airstair door and

emergency exitsAD FAR AC 12/1/03 7,427 8,045

2003-13-16 (08/25/2003) Aft Pressure

Bulkhead of FuselageAD FAR AC 12/1/03 7,427 8,045

2004-17-02 (10/04/2004) Cross shaft attach

boltSB 73-3634 AD FAR AC 11/24/04 7,802 8,471

2004-23-02 (12/23/2004) Nose Landing Gear

(NLG) Fork

Supersedes AD 87-22-

01 R1AD FAR AC 5/17/05 7,986 8,718

2004-23-02 (12/23/2004) Nose Landing Gear

(NLG) Forkn/a due to p/n change AD FAR AC 7/10/13 10,438 11,601

2005-01-04 (02/22/2005) Fuel hose AD FAR AC 5/17/05 7,986 8,718

2005-01-19 (02/23/2005) Garmin Mode S

transpondersAD FAR AC 1/24/12 10,091 11,227

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2005-18-20 (10/14/2005) Goodrich

"FASTprop" propeller de-icersNot installed AD FAR AC

2006-13-10 (08/07/2006) Rudder trim tab AD FAR AC 7/13/06 8,386 9,183

2006-16-18 R1 (07/18/2008) Sandel ST3400

TAWS/RMIAD FAR AC 9/9/08 9,160 10,085

2020-25-01 (01/11/2021) Wings PCW AD FAR AC 2/4/21 11,757 12,949

Left Engine PT6A-21 s/n PCE-24782

80-08-12 (04/18/1980) Fuel Pump Drive

Coupling SplinesPCW AD FAR LE 1/30/06 8,106

92-15-11 (08/17/1992) Compressor Delivery

Air Line (P3) Filter AssemblyPCW AD FAR LE 1/30/06 8,106

97-04-12 (03/14/1997) Compressor Bleed-off

ValveN/A AD FAR LE 1/30/06 8,106

2002-23-13 (12/31/2002) Turbine Exhaust

DuctsAD FAR LE 12/1/03 7,357 7,838

2014-11-05 (08/05/2014) Reinforcement liner

to the power turbine (PT) containment ring and,

for certain PT containment rings, adding scallops

AD FAR LE 4/15/15 10,651 11,631

Right Engine PT6A-21 s/n PCE-24783

80-08-12 (04/18/1980) Fuel Pump Drive

Coupling SplinesPCW AD FAR RE 11/16/05 8,060

92-15-11 (08/17/1992) Compressor Delivery

Air Line (P3) Filter AssemblyPCW AD FAR RE 11/16/05 8,060

97-04-12 (03/14/1997) Compressor Bleed-off

ValveN/A AD FAR RE 11/16/05 8,060

2002-23-13 (12/31/2002) Turbine Exhaust

DuctsAD FAR RE 12/1/03 7,371 7,884

2014-11-05 (08/05/2014) Reinforcement liner

to the power turbine (PT) containment ring and,

for certain PT containment rings, adding scallops

AD FAR RE 4/15/15 10,650 11,663

70-05-06 (03/11/1970) Blade N/A Blade Design AD FAR LP

72-08-04 (04/11/1972) Blades N/A Blade S/Ns AD FAR LP

74-14-01 (08/22/1974) Propeller blades N/A Blade Design AD FAR LP

83-08-01 R2 (05/11/2005) Propellers N/A by bolt P/N AD FAR LP

86-05-12 (06/27/1986) Pilot Tube N/A by Prop Model AD FAR LP

96-15-04 (07/29/1996) Propeller Blade Shank N/A Blade Design AD FAR LP

96-18-14 (10/16/1996) Hub N/A by Hub S/N AD FAR LP

2003-04-23 (04/04/2003) Propeller Blades N/A by Prop Model AD FAR LP

Left Propeller HC-B3TN-3B s/n BUA20404

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2003-13-17 (07/18/2003) Propeller blade N/A by Hub S/N AD FAR LP

2005-04-08 (03/29/2005) Blade pilot tube bore

areaN/A by Prop Model AD FAR LP

2005-14-11 (08/17/2005) Failed propeller

bladeN/A by Last RTS AD FAR LP

2005-14-12 (07/29/2005) Propeller mounting

boltsN/A by Bolts Lot No. AD FAR LP

2005-18-20 (10/14/2005) Goodrich

"FASTprop" propeller de-icersNot installed AD FAR LP

2006-24-07 (01/03/2007) Propeller blades N/A by prop S/N AD FAR LP

2009-10-14 (06/04/2009) Steel hub turbine

propellersN/A by Prop Model AD FAR LP

70-05-06 (03/11/1970) Blade N/A Blade Design AD FAR RP

72-08-04 (04/11/1972) Blades AD FAR AC 5/19/95 4,156

74-14-01 (08/22/1974) Propeller blades N/A Hub S/N AD FAR AC

83-08-01 R2 (05/11/2005) Propellers N/A by bolt P/N AD FAR RP

86-05-12 (06/27/1986) Pilot Tube AD FAR AC Inspect 5/17/05 7,986 8,718

96-15-04 (07/29/1996) Propeller Blade Shank N/A Blade Design AD FAR AC

96-18-14 (10/16/1996) Propeller hub AD FAR AC 3/5/99 5,758

2003-04-23 (04/04/2003) Propeller Blades N/A by Prop Model AD FAR RP

2003-13-17 (07/18/2003) Propeller blade AD FAR AC 7/13/06 8,386 9,183

2005-04-08 (03/29/2005) Blade pilot tube bore

areaN/A by Prop Model AD FAR RP

2005-14-11 (08/17/2005) Failed propeller

bladeN/A by Last RTS AD FAR RP

2005-14-12 (07/29/2005) Propeller mounting

boltsAD FAR AC 1/12/06 8,205 8,987

2005-18-20 (10/14/2005) Goodrich

"FASTprop" propeller de-icersNot installed AD FAR RP

2006-24-07 (01/03/2007) Propeller blades N/A by S/Ns AD FAR AC

2009-10-14 (06/04/2009) Steel hub turbine

propellersN/A by Prop Model AD FAR RP

Appliance ADs

87-06-09 - Mechanical Products circuit breakers AD FAR AC 11/18/09 9,531 10,563

98-25-10 R1 - Aircraft Belts, Inc. AD FAR AC 1/5/99

99-08-21 - Reduced oxygen consumption N/A AD FAR AC 10/4/99 6,014 6,376

2001-14-51 - Apollo SL30 VHFnav/comm AD FAR AC 12/1/03 7,427 8,045

2001-15-17 - CTL-92 transponedr control panel AD FAR AC 12/1/03 7,427 8,045

Left Propeller HC-B3TN-3B s/n BUA21991

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2002-06-06 - Rockwell TDR-94 transponders N/A by p/n AD FAR AC 3/15/11 9,903 11,033

2004-10-15 - Garmin International GTX

330/330D Mode S TranspondersAD FAR AC 11/24/04 7,802 8,471

2009-05-05 - Avidyne Primary Flight Displays AD FAR AC 11/18/09 9,531 10,563

2009-05-08 - Trimble or Freeflight Global

Positioning System (GPS) AD FAR AC 11/18/09 9,531 10,563

2010-01-03 (01/20/2010) Fire Fighting

Enterprises Limited Portable Halon 1211 Fire

Extinguishers

N/A by manufacture AD FAR AC 8/24/10 9,741 10,837

2010-04-16 (03/08/2010) SICLI Halon 1211

Portable Fire ExtinguishersN/A by manufacture AD FAR AC 8/24/10 9,741 10,837

2010-11-05 (07/06/2010) AVOX Systems and

B/E Aerospace Oxygen CylindersN/A by bottle size AD FAR AC 8/24/10 9,741 10,837

2014-18-01 (10/14/2014) Rockwell Collins,

Inc. Mode S TranspondersNot installed AD FAR AC

2015-10-51 (07/01/2015) Avidyne Corporation

Integrated Flight DisplaysNot installed AD FAR AC

2016-11-20 (07/15/2016) B/E Aerospace

Protective Breathing Equipment Part Number

119003-11

Not installed AD FAR AC 2/28/17 11,116 12,326

2017-04-06 (04/07/2017) United Instruments,

Inc. 5934 Series AltimetersN/A by Altimeter S/N AD FAR AC 2/20/18 11,295 12,495

2017-16-01 (10/24/2017) Ameri-King

Corporation Model AK-450-( ) and AK-451-( )

series emergency locator transmitters (ELTs)


2017-18-12 (10/16/2017) B/E Aerospace

Protective Breathing Equipment Part Number

119003-11 and 119003-21


2018-21-14 (03/27/2019) Zodiac Aerotechnics

Oxygen Mask RegulatorsNot installed AD FAR AC 2/13/20 11660 12853


Inc. (Rockwell Collins) Flight Display System

Application FDSA-6500

Not installed AD FAR AC 2/13/20 11660 12853

2019-13-03 (08/27/2019) Trig Avionics

Limited Mode S TranspondersNot installed AD FAR AC 2/13/20 11660 12853


Inc. Flight Management SystemsNot installed AD FAR AC

2020-18-51 (08/28/2020) Sandia Attitude

IndicatorNot installed AD FAR AC

SERVICE BULLETINS (as of 02/02/2021) SB

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MTB-24-01 - Enhanced Clearance for Pedestal

Wire HarnessesSB OSB AC 2/13/20 11,660 12,853

MTB-33-01 R1 - REPLACEMENT OF ENTRY

AND ICE LIGHT SOCKETSSB OSB AC

MTB-52-01 R1 - Inside Airstair Door Handle

Snap Ring ModificationSB RSB AC 2/15/19 11,500 12,638

MTL-21-01 - INSPECTION OF THE CABIN

ALTITUDE AND DIFFERENTIAL PRESSURE

AND THE CABIN RATE OF CLIMB

INDICATORS FOR INSTALLED SHIPPING

PLUGS

SB RSB AC 2/13/20 11,660 12,853

MTL-57-01 R1 - Lower Forward Wing Bolt

Crush Washer Inspection/ReplacementSB MSB AC 2/15/19 11,500 12,638

2028 R4 - Elevator trim tab system Part I SB MSB AC 7/17/84 1501

2028 R4 - Elevator trim tab system Part II SB MSB AC 7/17/84 1501

2028 R4 - Elevator trim tab system Part III Fwd cable guard Kit SB MSB AC 11/14/85 1783

2028 R4 - Elevator trim tab system Part IV SB MSB AC

2028 R4 - Elevator trim tab system Part V SB MSB AC

2028 R4 - Elevator trim tab system Part VI SB MSB AC

2028 R4 - Elevator trim tab system Part VII SB MSB AC

2028 R4 - Elevator trim tab system Part VIII SB MSB AC

2029 - Replacement of the Fuel Purge Tank and

Associated PlumbingSB OSB AC

2055 - Installation of Terminal Covers Over

Subpanel Feeder Diode TerminalsSB OSB AC

2057 R2 - Installation of an Improved Shoulder

Harness and Lap Belt Assembly on the Aft

Compartment Forward Facing Toilet

SB MSB AC

2066 R2 - Installation of an Improved Fuel Flow

Divider and Dump Valve AssemblySB OSB AC

2085 - Installation of an Improved Air

Conditioner Relay ControlSB OSB AC

2087 R1 - Improved Propeller Seal Drain

ProvisionsSB OSB AC

2108 R1 - Part I, Installation of Improved

Windshield Deice Circuitry; Part II, Installation

of Replacement Heated Windshields

SB OSB AC

2141 - Installation of a Camera Glass Defroster SB OSB AC

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2149 - Installation of Anti-Collision Beacon Kits SB OSB AC

2156 - Insp/Repl of fuel boost pumps SB MSB AC 1/24/12 10,091 11,227

2159 R2 - Replacement of Engine Oil Pressure

Transducers and Electrical ConnectorsSB OSB AC

2212 - Inspection of Flight Control Cable

TensionsSB MSB AC 3/16/88 2293

2213 R3 - Inspection of Pilot and Copilot Seat

Track WearSB MSB AC 10/27/88 2444

2220 - Inspection and/or Replacement of the

Nose Landing Gear Steering LinkSB MSB AC 5/31/90 2891

2231 R2 - Part I, Inspection of Elevator

Bellcrank Support Arm/Cable Rod End

Attachment Area

SB MSB AC 10/21/91 3186

2231 R2 - Part II, Inspection of Elevator

Bellcrank Assemblies For Corrosion and/or

Cracks

New bellcrank 50-

524401-11SB MSB AC 10/21/91 3186

2234 - Installation of Water Barrier In Nose

Avionics CompartmentSB OSB AC

2247 - Replacement of Emergency Exit Latch

BoltsSB MSB AC 12/8/89 2740

2248 - Part I, Inspection of Lower Forward

Inconel Wing Attachment Nuts for CracksAD 88-04-07 SB MSB AC 3/16/88 2293

2248 - Part II, Scheduled Replacement of Inconel

Wing Attachment NutsSB MSB AC 3/18/88 2293

2250 - Elimination of Radio Frequency

Interference Noise In Airplanes Equipped With

Sperry RD-550 HSI Indicators

SB OSB AC

2256 - Removal of scotch foam from Ailerons AD 89-22-14 SB MSB AC 8/2/02 7009 7524

2266 R1 - Announcement of Hartzell Propeller

Service Bulletin No. 159SB MSB AC 10/27/88 2444

2267 R2 - Part I, Removal of Ceramic Fiber

Paper and Inspection For Corrosion; Part II,

Optional Bleed Air Line Failure Warning System

Removal

SB MSB AC 5/31/90 2891

2276 - Installation of Inverter Replacement Kits SB OSB AC

2279 - Inspection of the Lower Forward Wing

Spar For Proper Rivet Spacing13,000 hrs / 3000 hrs SB MSB AC 13,000 4/4/80 0 0 1,196 13,000

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2280 - Inspection For Revision III of Service

Instructions 0867-341SB OSB AC

2312 - Inspection of Aft Fuselage Moisture

Drainage SystemAD 90-08-17 SB MSB AC 5/31/90 2891

2365 R1 - Addition of drain holes in rudder tab AD 92-07-05 SB MSB AC 2/18/91 3036

2405 - Inspection to Verify Installation and

Addition of All Interior and Exterior Placards

and Markings (RECURRING INSP)

SB OSB AC

2432 - Inspection/Replacement of the Engine

Mount Assembly Attachment BoltsAD 92-15-01 SB MSB AC 8/28/92 3334

2444 R2 - Inspection/Modification to the Pilot

and Copilot Chair Locking MechanismAD 97-06-06 SB MSB AC 5/14/97 4889

2455 - Installation of Stiffener Support Clips in

the Main Landing Gear Wheel WellsSB OSB AC

2475 - Part I, Inspection of the Leading Edge

Fuel Tank Inboard Nipples for Leaks; Part II,

Replacement of the Leading Edge Fuel Cell

Inboard Nipple to Main Spar Web Interconnect

Fuel Tube Assemblies

AD 93-17-01 SB MSB AC 3/10/93 3419

2484 R1 - Outflow/Safety Valve

Inspection/ReplacementSB OSB AC

2606 - Replacement of the Ventilation Blower SB OSB AC

2629 - Flap Rib Replacement SB OSB AC

2676 - Pressurization Control System Pneumatic

Tubing Inspection/RepairAD 97-23-17 SB MSB AC 5/14/97 4889

2695 - BFGoodrich Main Landing Asbestos

Brake Assembly Conversion KitsSB OSB AC

2718 R2 - Replacement of MIL-H-6000B Hose

Manufactured By Buckeye Rubber Products IncSB MSB AC 5/14/97 4889

01-4137 R1 - Removal of Capability to Operate

at Increased Gross Weight Above 10,100 lbsN/A SB MSB AC

01-4143 - Reinstatement of Capability to

Operate Above 10,100 lbsSB OSB AC

24-3181 - Generator Control Unit

Inspection/ReplacementSB RSB AC

24-3374 - Installation Of A Wet Drive Starter-

GeneratorSB OSB AC

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27-3459 R2 - Flight Control Gust Lock

Inspection/ReplacementAnnually SB MSB AC 12 2/4/21 11,757 12,949 6 Feb-22

28-3401 - Fuel Cell Cover And Gasket

InstallationSB RSB AC

28-3611 - FUEL VENT DEFLECTOR

INSTALLATIONSB OSB AC

28-4059 - Introduction of Improved Fuel Cell

GasketSB RSB AC 1/24/12 10,091 11,227

28-4059 R1 - Introduction of Improved Fuel Cell

Gasket

-9 gaskets installed

1/24/2012SB RSB AC

32-2102 R7 - Inspection/Replacement of Nose

Gear Lower Shock Absorber AssemblyAD 87-22-01 R1 SB MSB AC 200

32-3090 - Alternate Grease and Wheel Retention

Seal ModificationSB OSB AC

32-3116 - Main Landing Gear Torque Knee

ReplacementAD 2002-01-10 SB RSB AC 6/21/00 6331 6703

32-3134 R1 - Torque Knee Inspection AD 2002-01-10 SB MSB AC 6/20/98 5447

33-3410 - FLASHING BEACON HARDWARE

KIT IMPROVEMENTSB RSB AC 1/24/12 10,091 11,227

34-3236 - Y2K Software Anomaly SB RSB AC 10/4/99 6014 6376

52-3096 - NEW EXTERNAL DOOR

OPERATING INSTRUCTIONS PLACARDSB MSB AC 4/19/01 6625 7072

52-3096 R1 - NEW EXTERNAL DOOR

OPERATING INSTRUCTIONS PLACARD

P/C/W by originl issue.

No further action

required.

SB MSB AC

53-3105 - Inspection For Missing Rivets SB MSB AC 4/15/02 6923 7438

53-3513 - Aft Pressure Bulkhead Web

Inspection/RepairSB MSB AC 8/2/02 7009 7524

53-3513 R1 - Aft Pressure Bulkhead Web

Inspection/Repair

P/C/W by originl issue.

No further action

required.

SB MSB AC

55-2365 R2 - Addition of Drain Holes in the

Rudder TabSB MSB AC 1/12/06 8,205 8,987

55-3875 - Introduction of Improved Elevator

Trim Tab AssembliesSB OSB AC

56-3132 - COCKPIT SIDE WINDOW "D"

REPLACEMENTSB RSB AC

57-3148 - RIGHT AILERON SUB SPAR

INSPECTION/MODIFICATIONSB MSB AC 4/26/01 6625 7072

61-3737 - Propeller Mounting Bolt

Inspection/ReplacementSB MSB AC 1/12/06 8,205 8,987

71-3185 - Replacement Of The Fuel Purge Tank

And Associated PlumbingKit 109-9012-1 s/n 192 SB MSB AC 9/10/02 7021

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72-3461 - REPLACEMENT OF REAR

GOVERNOR HEATED AIR PRESSURE TUBE

(PY) ASSEMBLY

SB RSB AC

73-3634 - ENGINE CONTROLS CROSS

SHAFT/PEDESTAL MODIFICATIONSB MSB AC 12/1/03 7427 8045

SERVICE INSTRUCTIONS SI

0632-280 R1 - Inspection of Condition of Fuel

Cells and Possible Seepage of FuelSI C1 AC 5/10/85 1690

1140 - Inspection and/or Replacement of Wing

Attach Bolts, Nuts and Inspection of Wing

Attach Fittings

Inconel installed SI C1 AC

1158 - Inspection and Possible Rework of Lap

Belt and Shoulder Harness Assemblies

Manufactured By American Safety Equipment

Corporation

SI C1 AC 5/1/81 500

1160 - Inspection of the Landing Gear Retract

Gearbox and RH Torque Shaft For Proper

Alignment

SI C1 AC 5/1/81 500

1162 - Inspection and Possible Replacement of

the Outflow/Safety ValvesSI C1 AC 5/1/81 500

1163 - Inspection For Clearance Between the

Landing Gear Retract Chain and Air Conditioner

Wiring

SI C1 AC 5/1/81 500

1171 - Installation of a Secondary Latch

Mechanism On the Hinged Nose Baggage Door

Superseded by SI 1181

R1SI C1 AC 7/21/82 1002

1176 - Increase Clearance Between the Seatback

Pan and Shoulder HarnessSI C1 AC 7/1/81 588

1181 R1 - Installation of a Secondary Latch

Mechanism On the Hinged Nose Baggage Door SI C1 AC

1198 - Installation of an Improved Shoulder

Harness and Lap Belt Assembly on the Aft

Conmpartment Forward Facing Toilet

Superseded by SB 2057 SB C1 AC 6/7/84 1462

1208 - Inspection and/or Replacement of Wing

Attach Bolts, Nuts and Inspection of Wing

Attach Fittings

SI C1 AC 4/8/82 904

1211 - Inspection of the Landing Gear

Emergency Extension SystemSI C1 AC 11/24/82 1110

1213 R1 - Removal of Transzorbs From the

Avionics Bus RelaysSI C1 AC 7/21/82 1002

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1235 - Installation of Inconel Wing Attach Bolts

and Nuts and Inspection of Wing Attach FittingsSI C1 AC 6/7/84 1462

The information in this report is for planning purposes only and is not a maintenance tracking service. Central Flying Service, Inc. is not making any statement, actual or implied, as to

the value or airworthiness of the aircraft. All items should be verified by current aircraft records before any work is accomplished or decision made as to the maintenance status of the

aircraft.

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LJ-904 N94HB Status Report - Sandhills Global

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Transcript of LJ-904 N94HB Status Report - Sandhills Global