LLP Status Report - MyAirTrade

(OASES Option : TR42)

Report Date : 24Feb2020 08:50 Page : 1 ofLLP Status Report 4

Description Serial Number

Aircraft Reg

Part Number Install Date

LY-VEV

731335CFM56-5A ENGINECFM56-5A1/F 01Jun2018

CSN

AC CSN

62225:43

49043:58

TSN

32119

AC TSN

36637

MSN ManufacturedModel

Position

Last Flight

29Apr199100211A320-211

1000EM1

16Dec2019

Component Serial Life Interval Life At Install Life Since New % Due DatePart Life RemainingLimit

FAN AND BOOSTER ASSY

00:00

000

74.97BD020340336-014-808-0BOOSTER SPOOL

2249122491

31169863:39

7509679

68303000030000

DateDays (Calendar)HoursLandingsCFM56-5A1/F CyclesCFM56-5A3 Cycles

Lifed PartsDiscard

00:00

000

67.59PA353529336-018-105-0FAN DISK

1689715545

31169863:39

7509679

68302500023000


Lifed PartsDiscard

#1 AND #2 BRG SUPPORT ASSY

00:00

000

74.97DD104339335-006-414-0FAN SHAFT

224912249122491

31169863:39

7509679

6830

300003000030000


Lifed PartsDiscard

Created by


Aircraft Reg


LY-VEV


CSN

AC CSN

62225:43

49043:58

TSN

32119

AC TSN

36637


Position

Last Flight

29Apr199100211A320-211

1000EM1

16Dec2019

LLP Status Report Report Date : 24Feb2020 08:50 Page : 2 of 4


HP COMPRESSOR ROTOR ASSY

00:00

0000

36.05GWN0F03D1386M56P03HPC ROTOR FWD SHAFT

7210721072107210

456918260:43

127902688

6799423

20000200002000020000

DateDays (Calendar)HoursLandingsCFM56-5A1 CyclesCFM56-5A1/F CyclesCFM56-5A3 Cycles

Lifed PartsDiscard

018854:00

78004872

00

2928

40.27GWN030D91558M31G04HPC ROTOR SPOOL, STG1 AND 2

80538053805380538053

456924639:14

119474872

67934682928

2000020000200002000020000

DateDays (Calendar)HoursLandingsCFM56-5A1 CyclesCFM56-5A1/F CyclesCFM56-5A3 CyclesCFM56-5A5 Cycles

Lifed PartsDiscard

00:00

000

62.46XAES58731590M59P01HPC ROTOR DISK, STG3

124911249112491

31169863:39

7509679

6830

200002000020000


Lifed PartsDiscard

00:00

000

62.46GWN0M7W81588M89G03HPC ROTOR SPOOL, STG4-9

124911249112491

31169863:39

7509679

6830

200002000020000


Lifed PartsDiscard

020813:00

101164492

05624

45.96GFF5D8MP1359M86P03CDP ROTATING AIRSEAL, REAR

919191919191

456922707:15

108094492

6795638

200002000020000


Lifed PartsDiscard

Created by


Aircraft Reg


LY-VEV


CSN

AC CSN

62225:43

49043:58

TSN

32119

AC TSN

36637


Position

Last Flight

29Apr199100211A320-211

1000EM1

16Dec2019

LLP Status Report Report Date : 24Feb2020 08:50 Page : 3 of 4


HP TURBINE ROTOR ASSY

00:00

0000

36.05XAE564781386M80P05HPT ROTOR SHAFT, FWD

721072107210

456918260:43

127902688

6799423

200002000020000


Lifed PartsDiscard

09476:00

56430

5643

62.85TMT3TA361863M77P01HPT ROTATING AIRSEAL, FWD

1118811188

456911610:30

6612679

59331780017800


Lifed PartsDiscard

00:00

0000

26.07GATHJ7FP1319M13P08HPT ROTOR DISK

451045104510

456918260:43

127902688

6799423

173001730017300


Lifed PartsDiscard

010693:00

97539753

00

45.02TMTTD1541864M89P02HPT REAR SHAFT

877887788778

456912827:43

107229753

679290

195001950019500


Lifed PartsDiscard

Created by

(OASES Option : RC20)

Report Date : 21Feb2020 12:37 Page : 1 ofAD/EAD Statement 18

LY-VEV

Aircraft Reg MSN Airframe TSN

A320-211 49043:58

Model

36637

Airframe CSN

00211

Manufacture Date Last Flight

16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-F-1991-243-EASA AIRBUS - CFM 56-5 Electrical Harnesses 13Nov1991 71

CommentsPart / Serial: CFM56-5A1/F / 731335Pos / Zone: 1000EM1 / 4.1

Method Of Compliance Life Limit/Interval

LastComplR Next

Due RemainParagraph F/ LE/DO/Ride

(1) Visually inspect the electrical harnesses partnumber 238W0904-509, 238W0904-511 and238W0908-511 and perform draining provisionin accordance with AIRBUS INDUSTRIE ALLOPERATORS TELEX reference AOT 71-01 rev 1dated October 22, 1991.

Not ApplicableQEC S/N Q731335 installed

(2) (a) Remove and modify the electrical harnessesiaw AIRBUS INDUSTRIE ALL OPERATORS TELEXAOT 71-01 rev 1 dated October 22, 1991 within600 flight hours if humidity or corrosion wasdetected during the visual inspection.


(2) (b) Remove and modify the electrical harnessesiaw AIRBUS INDUSTRIE ALL OPERATORS TELEXAOT 71-01 rev 1 dated October 22, 1991 within3000 flight hours if neither humidity norcorrosion was detected during the visualinspection.


Title Eff DateRef No(s) ATAAD-F-1994-099-EASA Engine Starting - Air Starter - Modification 07May1994 71

CommentsEquivalent To: AD-FAA AD 97-05-13-FAAPart / Serial: CFM56-5A1/F / 731335Pos / Zone: 1000EM1 / 4.1


LastComplR Next


- The starter shall be modified (except if alreadydone) per SB CFM 56-5 N° 80-003 dated July16, 1994 (or any later approved revision orequivalent).

N/A by P/N installedP/N 3505582-45 Installed

Created byForm 10 Rev 2

AD/EAD Statement Report Date : 21Feb2020 12:37 Page : 2 of 18

LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-F-1994-272R3-EASA Engine - High Pressure Compressor 1-2 Spool - Inspection / Replacement 07Oct1995 72

CommentsEquivalent To: AD-97-06-01-FAAPart / Serial: CFM56-5A1/F / 731335Pos / Zone: 1000EM1 / 4.1


LastComplR Next


(A) Inspect the stage 1 disk bores and then re-inspect within every 2200 cycles since the lastinspection iaw the instructions of applicable S.B.Remove those spools with rubbed and/orscratched stage 1 disk bores from service forpiece part inspection and possible rework.

N/A by SB Effectivitynot listed in sb effectivity

(B) Remove from service at the next shop visit onthe effective date of this ADN°3 bearing aft air/oil seal P/N 1364M71G02and replace with seal bearing an approved P/N; spools 1-2 identified with rubbing and/orscratch indications must be removed orrepaired at this opportunity.

N/A by SB Effectivitynot listed in sb effectivity

Title Eff DateRef No(s) ATAAD-F-1989-181R3-EASA Engine - No.3 Bearings - Inspection / Replacement 27Jan1996 72

CommentsEquivalent To: AD-FAA AD 89-23-06 R1-FAAPart / Serial: CFM56-5A1/F / 731335Pos / Zone: 1000EM1 / 4.1


LastComplR Next


(A) to (F) Inspect the forward sump magnetic plug chipdetector.

N/A by Equipment not installedBearing P/N 1364M91P01 introduced from production

(A-2) and(B-2)

Remove from service number 3 bearings. N/A by Equipment not installedBearing P/N 1364M91P01 introduced from production



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-F-1997-010R1-EASARevision: 1 / 26Feb1997

Engine - Low Pressure Turbine Rotor Stub Shafts and Conical Supports - Life Limits 08Mar1997 72



LastComplR Next


(A) and (B) Reidentify CFM 56-2A / CFM 56-2B LPTR stubshafts.

N/A byN/A by Engine Type

(C), (D)and (E)

Reidentify CFM 56-2 / CFM 56-2A / CFM 56-2BLPTR conical supports


(F) Reidentify CFM 56-3 /-3B /-3C LPTR stub shafts. N/A byN/A by Engine Type

(G) Reidentify CFM 56-3 /-3B /-3C LPTR conicalsupports.


(H) Remove from service CFM 56-5 LPTR conicalsupport, P/N 336-000-305-0

N/A byP/N 338-077-502-0 Installed

Title Eff DateRef No(s) ATAAD-F-1998-097-EASA Engine - Accessory Gearbox Gearshaft Cluster Spur Assembly - Replacement 25Feb1998 72



LastComplR Next


(3-a,b,c) a) Remove from service the gearshaft clusterspur assy (31x71 teeth) in the accessory gearbox (AGB) of engines in the above lists 1A and1B. (See SB CFM56-5 S/B 72-523 Rev 1) underthe schedule of paragraph 4 hereafter.b) Remove from service the gearshaft clusterspur assy (31x71 teeth) in the accessory gearbox (AGB) of engines in the above lists 2A and2B. (See SB CFM56-5B S/B 72-211 Rev 1)under the schedule of paragraph 4 hereafter.c) Remove from service the gearshaft clusterspur assy (31x71 teeth) in the accessory gearbox (AGB) of engines in the above lists 3A and3B. (See SB CFM56-5C S/B 72-350 Rev 1)under the schedule of paragraph 4 hereafter.

N/A by S/N installedSN UR0064 installed



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-F-1998-334-EASA Time Limits / Maintenance Checks - High Pressure Turbine Front Air Seal - Life Limi

Reduction22Aug1998 72



LastComplR Next


- IMPLEMENTATION OF NEW LIFE LIMITS N/A by P/N installedP/N 1863M77P01 Installed

Title Eff DateRef No(s) ATAAD-F-1998-427R2-EASARevision: 2 / 20Oct1999

Engine Fuel & Control - Fuel Filter Cover Attachment Parts - Inspection 31Dec1999 73



LastComplR Next


(3.1) Perform once all accomplishment instructionsof paragraph 2 of SB CFM56-5 73-136 Rev. 2dated April 29, 1999 or CFM56-5B 73-056 Rev2 dated April 29, 1999 or CFM56-5C 73-073Rev. 2 dated April 29, 1999.


(3.2) Perform SB CFM56-5 A73-143, CFM56-5B A73-062, CFM56-5C A73-078. N/A by P/N installed

P/N 714900-5 Installed

Title Eff DateRef No(s) ATAAD-2000-15-01-FAA Fuel Leakage 73



LastComplR Next


- Paragraph Not Defined Not ApplicableP/N 714900-5 S/N 27652 installed



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-F-2001-177-EASA Engine Starting - Starter Bayonet Oil Plug - Replacement 26May2001 80



LastComplR Next


- Perform once all accomplishment instructionsof SB CFM56-5 80-014 Rev 2 dated November17, 2000 (or later approved revision), orCFM56-5B 80-006 Rev 2 datedNovember 21, 2000 (or later approvedrevision), or CFM56-5C 80-009 Rev 2 datedNovember 21, 2000 (or later approvedrevision).


Title Eff DateRef No(s) ATAAD-F-2001-207-EASA SUPERSEDED BY DGAC FRANCE AD 2001-240 30May2001 72



LastComplR Next


- Paragraph Not Defined Superseded By: AD-F-2001-240-EASA On 23Jun2001

Title Eff DateRef No(s) ATAAD-F-2001-240-EASA Aft Sump Magnetic Chip Detector Inspection / Number 4 Bearing Replacement 23Jun2001 72

CommentsEquivalent To: AD-2001-11-05-FAASupersedes: AD-F-2001-207-EASAPart / Serial: CFM56-5A1/F / 731335Pos / Zone: 1000EM1 / 4.1


LastComplR Next


(3.1) 3.1.1. For CFM56-2B, CFM56-2, CFM56-3 andCFM56-7 without DMS option inspect the aftsump Magnetic Chip Detector.3.1.2. For CFM56-5B check the ElectronicMagnetic Chip Detector indication.3.1.3. For CFM56-5C after each flight check forthe presence of class 2 fault messages"magnetic chip detected" through aircraftsystem as long as the No. 4 bearing has notbeen replaced.3.1.4. For CFM56-7B with DMS option checkFMC-MCDU for message 79-21141 or 79-21142.

N/A byEngine Type

(3.2) Replace the No. 4 bearing. Not Applicable



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-F-1998-003R3-EASA Engine - Low Pressure Turbine Casing Life Limit 22Dec2001 72



LastComplR Next


- Paragraph Not Defined N/A byEngine model

Title Eff DateRef No(s) ATAAD-2002-02-13-FAA Magnetic Drain Plug 72



LastComplR Next


- Paragraph Not Defined Not ApplicableP/N 3505582-45 INSTALLED

Title Eff DateRef No(s) ATAAD-F-2002-390-EASA Critical Life-limited Rotating Engine parts 01Aug2002 72



LastComplR Next


(a) Revise the Airworthiness Limitations Section(chapter 05-00-00) of Engine Shop Manual(ESM) CFMI-TP.SM.4, for CFM56-2 seriesengines, ESM CFMI-TP.SM.6, for CFM56-2A/-2Bseries engines, ESM CFMI-TP.SM.5, for CFM56-3/-3B/-3C series engines, ESM CFMI-TP.SM.7 forCFM56-5 series engines, ESM CFMITP.SM.9 forCFM56-5B series engines, ESM CFMI-TP.SM.8for CFM56-5C series engines, andESM CFMI-TP.SM.10 for CFM56-7B seriesengines, and for air carrier operations, revisethe approved continuous airworthinessmaintenance program.

Open



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-F-2002-470-EASA Second and Third Stage Low Pressure (LP) Turbine Nozzle Segments 28Sep2002 72



LastComplR Next


(3) The stage 2 LP turbine nozzle segmentsreferences 338-109-104-0, 338-109-105-0,338-109-106-0, 338-109-204-0, 338-109-205-0, 338-109-206-0, 338-109-304-0, 338-109-305-0, 338-109-306-0 and the stage 3 LPturbine nozzle segments references 338-109-702-0, 338-109-802-0 currently in service shallbe replaced.

N/A byEngine Type

Title Eff DateRef No(s) ATAAD-F-2004-095-EASA Engine Fuel & Control - Main Fuel Pumps equipped with Solid Bronze Bearings - Replacement 03Jul2004 73



LastComplR Next


(3) Replace main fuel pumps equipped with solidbronze bearings with pumps equippedwith bi-metal aluminium/bronze bearings.




LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-F-2003-456R2-EASARevision: 2 / 29Sep2004

Starting - Air Turbine Starter - Rework 09Oct2004 80

CommentsEquivalent To: AD-2005-10-05-FAASupersedes: AD-F-2003-422-EASAPart / Serial: CFM56-5A1/F / 731335Pos / Zone: 1000EM1 / 4.1


LastComplR Next


(3) Rework the air turbine starter, N/A by Equipment not installedP/N 3505582-45 Installed

Title Eff DateRef No(s) ATAAD-F-2003-001R2-EASARevision: 2 / 08Jun2005

Engine indicating - EGT harnesses and couplings 18Jun2005 72



LastComplR Next


(3)- beingtrend

monitored

Review the smooth data EGT trend via theSystem for Analysis of Gas Turbine Engines(SAGE) or equivalent.If this monitoring shows a 30°C (or more)downward (i.e. cooler) temp indication shiftwithout a corresponding change in otherassociated engine parameters such as N1 (LProtor speed), N2 (HP rotor speed) and fuel flow,replace the EGTharnesses and couplings provided that there issufficient actual EGT margin.Continue to monitor the EGT indications for3,000 hours time since the firstinstallation on the current engine.

N/A by Equipment not installedP/N CA146-01, CA147-00, CA148-00 Installed

(3)-notbeingtrend

monitored

For affected EGT harnesses and couplings, withless than 3,000 hours since installation and notbeing trend monitored replace affected EGTharnesses and couplings.

N/A by Equipment not installed



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-US-2006-26-01-FAA Engine Fuel & Control - Fuel Filters (PMA Parts) - Replacement 03Jan2007 73



LastComplR Next


(f) For CFM56-7B engines, replace fuel filter,Western Filter P/Ns WF337661 or WF337017and PTI Technologies P/Ns 7595983-101 or7588133, with a filter that has a P/N not listedin this AD.

N/A by P/N installed

(g) For CFM56-2 series, -3 series, and -5 seriesengines, replace fuel filter, Western Filter P/NsWF337661 or WF337017 and PTI TechnologiesP/Ns 7595983-101 or 7588133, with a filterthat has a P/N not listed in this AD.

N/A by P/N installed

Title Eff DateRef No(s) ATAAD-2007-0036R1-EASARevision: 1 / 27Feb2007

Power Plant - Forward Engine Mount Bolts - Inspection / Replacement / Retorque 16Feb2007 71



LastComplR Next


(1) It is the responsibility of the operators toensure that:-any maintenance on the engine mounts isperformed iaw correct instructions as identifiedin the AIRBUS AOT A320-71A1042 Rev 01and/or Goodrich AOL CFM56-074 Rev 1, orlater approved revisions; and-any forward engine mount support assembliesfitted on an engine which is used asreplacement has been fitted iaw correctinstructions as identified in the AIRBUS AOTA320-71A1042 Rev 01 and/or Goodrich AOLCFM56-074 Revision 1, or later approvedrevisions;

N/A byDate of installation



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-2007-0036R1-EASARevision: 1 / 27Feb2007

Power Plant - Forward Engine Mount Bolts - Inspection / Replacement / Retorque 16Feb2007 71



LastComplR Next


(2) For any forward engine mount supportassembly that has been installed ormaintained since May 2006 using theerroneous values given in the referencedmaintenance documents, or where use of thecorrect values cannot be established,accomplish the following iaw instructions ofAIRBUS AOT A320-71A1042 Rev 01 and/orGoodrich AOL CFM56-074 Rev 1:-Remove, inspect and discard the followingforward engine mount bolts 77710-5H6 (AMMitem 90) and NAS2815C15H (AMM item 85)where necessary.-If any bolts 77710-5H6 (AMM item 90) arefound broken during the above inspection,replace the affected forward engine mountsupport assembly (AMM item 75).-Replace bolts 77710-5H6 (AMM item 90) andNAS2815C15H (AMM item 85) with new itemsand torque them to the correct value wherenecessary.-Re-torque 77458-7H21 bolts (AMM item 95)and NAS2816C7H (AMM item 50) to the correctvalue.

N/A byDate of installation



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-2007-0221-EASA Time Limits - Low Pressure Turbine Rear Frame - Life Reduction 27Aug2007 72



LastComplR Next


(1) For LPT rear frame P/N 338-171-703-0, 338-171-704-0, 338-171-705-0, 338-171-706-0,comply with the LCF life limits iaw the chapters05-12-04, 05-12-24 and 05-21-03 in theCFM56-5B ESM, rev 47, dated January 15,2007, or later approved revision.

N/A byEngine Type

(2) If the number of cycles accumulated since newby a LPT rear frame P/N338-171-703-0, 338-171-704-0, 338-171-705-0, 338-171-706-0 cannot beestablished, remove and replace the LPT rearframe, or perform the inspections iaw CFM56-5B S/B 72-0620 initial issue, or later approvedrevision.

N/A byEngine Type

Title Eff DateRef No(s) ATAAD-2009-0110-EASA Time Limits - Low Pressure Turbine Rear Frame - Life Limit / Mandatory Inspection 21May2009 72



LastComplR Next


(1) Amend the approved operator maintenanceprogramme to incorporate the newLCF life limits or mandatory inspections for LPTrear frame P/N 338-171-751-0 and 338-171-752-0, iaw the CFM56-5B ESM chapter 05Temporary Revision (TR) 05-0186, 05-0187and 05-0188 applicable to the Engine ShopManual Rev 52 or iaw subsequent revisions ofthe Engine Shop Manual that incorporate theseTemporary Revisions.

N/A byEngine Type



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAEAD-2009-0154-E-EASA Engine Fuel and Control - Hydromechanical Unit (HMU) - Inspection / Replacement 17Jul2009 72



LastComplR Next


- Paragraph Not Defined Not Applicable

Title Eff DateRef No(s) ATAAD-2009-0270-EASA Engine - LPT Rotor / Stator Assembly - Replacement 31Dec2009 72



LastComplR Next


- Paragraph Not Defined N/A by S/N installedS/N BC281282 Installed

Title Eff DateRef No(s) ATAAD-2009-0088R1-EASARevision: 1 / 17Aug2010

[Correction] Engine - High Pressure Compressor (HPC) - Inspection / Replacement 08May2009 73

CommentsEquivalent To: AD-2010-09-14-FAAReferences: EAD-2008-0227-E-EASASupersedes: EAD-2008-0228-E-EASAPart / Serial: CFM56-5A1/F / 731335Pos / Zone: 1000EM1 / 4.1


LastComplR Next


- Paragraph Not Defined N/A byEngine Type



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-2010-0212-EASA Engine - Fan Blade - Replacement 01Nov2010 72



LastComplR Next


(1) For aeroplanes on which the affected fanblades are installed on both engines replacethe affected blades with serviceable blades iawCFM International Service Bulletin (SB) CFM56-5B S/B 72-0777.

N/A byEngine Type

(2) For aeroplanes on which the affected fanblades are installed on one engine only replacethe affected blades with a serviceable bladeiaw CFM International SB CFM56-5B S/B 72-0777.

N/A byEngine Type

Title Eff DateRef No(s) ATAAD-US-2009-11-02-FAA [Correction] High-Pressure Compressor (HPC) 4-9 Spools Improperly repaired by Propulsion

Technology LLC (PTLLC)23Jun2009 72



LastComplR Next


(f) Remove HPC 4-9 spools from service that havea P/N and S/N listed in this AD.

N/A byP/N 1558M89G03, S/N GWN0M7W8 Installed



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-2012-0123-EASA Engine Fuel and Control - Hydro-Mechanical Units - Operational Limitation 23Jul2012 72



LastComplR Next


- Paragraph Not Defined Superseded By: AD-2017-0065-EASA On 03May2017

Title Eff DateRef No(s) ATAAD-2014-0083-EASA Engine - Repaired Low Pressure Turbine Stage 1 Nozzle Segments - Identification /

Replacement16Apr2014 72

CommentsSupersedes: AD-2013-0183-EASAPart / Serial: CFM56-5A1/F / 731335Pos / Zone: 1000EM1 / 4.1


LastComplR Next


(1) Identify any nozzle vane segment that hasbeen repaired using AFR repair, ChromalloyNevada DER-N068 (04-CNV-068-0) or DER-N080 (06-CNV-080-0) and, before release toservice of the engine, replace each part with aserviceable part, in accordance with theinstructions of CGT SB 72-047 Revision 01.

Not ApplicableVane Replacement has not been performed

Title Eff DateRef No(s) ATAAD-2014-0130-EASA Time Limits - Engine Stationary Parts - Life Limits / Mandatory Inspections 03Jun2014 05



LastComplR Next


(1) and (2) Identify each life limited stationary partinstalled on an engine which was previouslyoperated in different engine modelconfiguration.If an engine stationary part is identified thathas previously been operated in a differentengine type or different engine model(including differentconfiguration, thrust rating), calculate theremaining life of each engine stationary partiaw the instructions of CFM56-5B ESM pageblock 05-12-00,as amended iaw TR 05-0223, or CFM56-7B ESMpage block 05-12-00, as amended iaw TR 05-0163, as applicable to engine type.

N/A byEngine Type



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-2016-0010R1-EASARevision: 1

CFM56 Powerplant - Aft Engine Mount Retainers - Inspection / Replacement 18Feb2016 71

CommentsReferences: SB-A320-71-1060-AIRBUS

SB-A320-71-1070-AIRBUSSupersedes: AD-2015-0021-EASAPart / Serial: CFM56-5A1/F / 731335Pos / Zone: 1000EM1 / 4.1


LastComplR Next


(1) and (2) Restatement of the requirements of EASA AD2015-0021:Accomplish a DET of the aft engine mountinner retainers in accordance with theinstructions of Airbus Alert OperatorsTransmission (AOT) A71N001-12 Revision 01.

Superseded By: AD-2017-0138-EASA On 16Aug2017

(6) Accomplish a DET of the aft engine mountinner retainers in accordance with theinstructions of Airbus SB A320-71-1060, orGoodrich Aerostructures SB RA32071-160.


(9) Identify each engine mount inner retainer inaccordance with the instructions of SB A320-71-1070 and replace each part that meets anyof the criteria as specified in paragraph (9.1),(9.2) or (9.3) of this AD, as applicable.


Title Eff DateRef No(s) ATAAD-2016-0039-EASA Engine - Low Pressure Turbine Rear Frames - Inspection / Replacement 01Mar2016 72



LastComplR Next


(1) Accomplish an on-wing or in-shop eddy currentinspection (ECI) or a fluorescent penetrantinspection (FPI) of the mount struts of eachTRF having P/N 338-102-907-0 or P/N 338-102-908-0, as applicable, installed on the LPTassembly, in accordance with the instructionsof paragraph 3.B (ECI) or paragraph 3.C (FPI) ofthe SB.

N/A byEngine Type

(2) Re-inspect the engine in accordance with theinstructions of paragraph 3.B (ECI) orparagraph 3.C (FPI) of the SB.

N/A byEngine Type



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-2017-05-09-FAA Remove the RDS assembly, part number

(P/N) 305-165-101-0, and RDS outer housing, P/N 301-295-106-0, and replace with partseligible forinstallation.

13Apr2017 72

CommentsEquivalent To: AD-2017-0084-EASAPart / Serial: CFM56-5A1/F / 731335Pos / Zone: 1000EM1 / 4.1


LastComplR Next


- Paragraph Not Defined N/A by S/N installedS/N UR01838 Installed sicce assembly date

Title Eff DateRef No(s) ATAAD-2017-0065-EASA Engine Fuel and Control - Hydro-Mechanical Units - Operational Limitations 03May2017 72

CommentsEquivalent To: AD-2013-14-06-FAASupersedes: AD-2012-0123-EASAPart / Serial: CFM56-5A1/F / 731335Pos / Zone: 1000EM1 / 4.1


LastComplR Next


(1) 1. Determine whether the HMU is, or has been,operated using TS-1 fuel2. Determine the engine hours accumulated byeach affected HMU, since first installation onan engine, since last HMU overhaul, and sincelast maintenance on the HMU

Not ApplicableNever operated using TS-1 fuel

(2) For an affected engine before the affectedHMU exceeds 10 000 engine hours since firstinstallation on an engine, or since last HMUoverhaul, or since last maintenance, or within3 months after the effective date of this AD,whichever occurs later, replace the HMU with aserviceable part

Not ApplicableNever operated using TS-1 fuel



LY-VEV


A320-211 49043:58

Model

36637

Airframe CSN

00211


16Dec201929Apr1991

Title Eff DateRef No(s) ATAAD-2017-14-08-FAA CFM56-3, 3B, -3C ENGINES HPC STATOR CASE CHECK 18Aug2017 72



LastComplR Next


1 Inspect to determine if the compressor frontstator case is marked with "RP031". If the caseis not marked with "RP031," Perform an initialpull force check of stage 1, 2 and 3 of thecompressor variable stator vane (VSV)actuation system.

Not Applicableapplicably only for CFM56-3 engines.

N/A for current engine

2 continue to perform repetitive pull forcechecks of stages 1, 2, and 3 of the compressorVSV actuation system and disposition asspecified in paragraphs (2)(i) through (iii) ofthis AD.



3 COMPRESSOR CASE IS FOUND MARKED"RP031"; NO FURTHER ACTIONS IS REQUIREDBY AD 2017-14-08



Title Eff DateRef No(s) ATAAD-2017-0138-EASA CFM56 Aft Engine Mounts Retainers - Inspection / Replacement 16Aug2017 71

CommentsSupersedes: AD-2016-0010R1-EASAPart / Serial: CFM56-5A1/F / 731335Pos / Zone: 1000EM1 / 4.1


LastComplR Next


2 accomplish a DET of the aft engine mountinner retainers in accordance with theinstructions of Airbus SB A320-71-1060, orGoodrich Aerostructures SB RA32071-160.

Superseded By: AD-2017-0251-EASA On 29Dec2017

THIS TASK REQUIRES ENGINE DROP9-10 Modify the aft engine mount assembly, havinga P/N identified as "Old" in Table 1 of this AD,and re-identify it with the corresponding P/Nidentified as "New" in Table 1 of this AD, inaccordance with the instructions of Airbus SBA320-71-1071.

Superseded By: AD-2017-0251-EASA On 29Dec2017


_____________________________________________________________________________________________________________________

Report Date: 19/11/19 Page 1 of 11

ENGINE CONDITION MONITORING

A320-211 LY-VEV MSN 211

Oct 2019

Prepared by / Checked by

Robert Bauer / Tadas Mačiulskis

Engine No. 1 CFM56-5A1/F

S/N 731335

LSV date 14-Sep-2017

LSV TSN 60.332 FH

LSV CSN 31.426 FC

Engine TSN 62.111 FH

Engine CSN 32.080 FC

EGT Margin 53°

Engine No. 2 CFM56-5A1/F

S/N 731200

LSV date 18-Feb-2015

LSV TSN 62.959 FH

LSV CSN 28.248 FC

Engine TSN 70.485 FH

Engine CSN 31.617 FC

EGT Margin 13°

__________________________________________________________________________________________________________________________

Fleet Performance Report Oct 2019 (last data point: 04.11.2019)

________________________________________________________________________________________________________________________________


Parameter Development

A/C #1 ESN EGT Oil, PSI Vibrations Date Comments / AOG / Report / Failure

LY-VEV 731473 13° N/A ~3 27.11.15 EGT: Engine Wash & Troubleshooting required / Vibration troubleshooting required

14° 50 ~3 02.01.16 EGT: Engine Wash & Troubleshooting required / Vibration troubleshooting required

15° 52 ~1,5 01.02.16 Fan Vib. Back to normal – EGT Margin ~15° - Engine Wash?

13° N/A ~1,5 25.02.16 If wash was performed: EGT Sys Troubleshooting required.



13° N/A ~1,5 31.05.15 Negative trend stopped – on watch

21° N/A ~1,5 30.06.15 None

14° 49 ~1,5 31.07.16 EGT Margin to be monitored

13° 49 ~1 31.08.16 EGT Margin to be monitored

18° 49 ~2 30.09.16 EGT recovered

17° 49 ~1 31.10.16 None

11° 49 ~2 30.11.16 EGT Margin to be monitored

10° 43 (CR) ~3 31.12.16 EGT Margin to be monitored

15° N/A ~1 31.01.17 EGT Stabilized

22° N/A <2 28.02.17 None

17° 47 (CRZ) <2 31.03.17 EGT Margin stable at low value

20° 49 (CRZ) <2 30.04.17 EGT Margin stable at low value

33° 54 (TO) ~1 31.05.17 None

25° 54 (TO) ~1 30.06.17 None – N1 vibration level not stable – Mid span shroud lubrication should be performed

27° 53 (TO) 1,5 31.07.17 None – N1 vibration level not stable – Mid span shroud lubrication should be performed

N/A N/A N/A 31.08 – 31.10.17

No Ops

41° 54 (TO) <1 31.12.17 None – to be monitored (Engine too good)

40° N/A ~1 31.01.18 None – to be monitored (Engine too good)

36° N/A ~1,5 28.02.18 None

__________________________________________________________________________________________________________________________


________________________________________________________________________________________________________________________________



44° N/A ~1,3 31.03.18 None

33° N/A 1,6 30.04.18 Engine to be removed due to internal oil leak

N/A N/A N/A 31.05.18 No flights in May – Dual Engine Chg.

Eng. Chg. 731335 64° N/A <1 30.06.18 None

62° N/A ~2 31.07.18 None

60° 43 (CRZ) 1,9 31.08.18 None

64° N/A 2,5 30.09.18 None – Fan Trim Balance required

65° 45 (CRZ) 2,4 31.10.18 None – Fan Trim Balance required

61° 44 (CRZ) 1,3 30.11.18 None

52° 47 (CRZ) ~1 31.12.18 None

60° 43 (CRZ) ~1 31.01.19 None

60° 44 (CRZ) <1 28.02.19 None (Note: Core Vibs – check vibration sensor)

60° 42 (CRZ) 1,3 31.03.19 None

60° 42 (CRZ) <1 30.04.19 None

58° 45 (CRZ) <1 31.05.19 None – Core Vib increase (>2) – Could be linked to pickup – see 1 Year trend. Boro should be considered (HPC, HPT)

58° 43 (CRZ) <1 30.06.19 None – Core Vib increase (>2) – Could be linked to pickup – see 1 Year trend. Boro should be considered (HPC, HPT)

56° 42 (CRZ) <1 31.07.19 None – Core Vibs 1,5 – on watch



53° 46 (CRZ) ~1 31.10.19 None – Core Vibs 1,2 – on watch (coming down)

__________________________________________________________________________________________________________________________


________________________________________________________________________________________________________________________________



LY-VEV 731200 25° N/A <2 27.11.15 None

24° 50 ~1 02.01.16 None

26° 52 ~1 01.02.16 None

22° N/A ~1,5 25.02.16 None

23° N/A ~1,5 31.03.16 None

22° N/A ~1 30.04.16 None

20° N/A ~1 31.05.16 EGT Margin - "Big scatter" - on watch

29° N/A <1 30.06.15 None

27° 51 <1 31.07.16 None

22° 50 <1 31.08.16 None

22° 49 ~1 30.09.16 None

23° 49 ~1 31.10.16 None

25° 49 <2 30.11.16 None

13° 44 (CR) <2 31.12.16 EGT Margin Drop (must be linked to operation - no N2 change)

13° N/A ~1 31.01.17 EGT Margin still low – to be monitored

15° N/A ~1 28.02.17 EGT Margin still low – to be monitored

13° 47 (CRZ) ~1 31.03.17 EGT Margin stable at low value

15° 50 (CRZ) ~1 30.04.17 EGT Margin stable at low value

26° 60 (TO) ~1 31.05.17 None

21° 60 (TO) ~1 30.06.17 None

25° 59 (TO) <1 31.07.17 None

N/A N/A N/A 31.08 – 31.10.17

No Ops

Eng. Chg. 731834 ~0° 59 (TO) 1,5 31.12.17 Run Out Eng. of LY-COM – To be monitored (LH engine too good)

2° N/A ~1 31.01.18 Run Out Eng. of LY-COM – To be monitored

-10° N/A ~1,5 28.02.18 Run Out Eng. of LY-COM – To be monitored (No DMU Data)

-12° N/A ~1,5 31.03.18 Run Out Eng. of LY-COM – To be monitored (No DMU Data)

-25° N/A 1,8 30.04.18 Engine to be removed due to EGT margin & internal oil leak

N/A N/A N/A 31.05.18 No flights in May – Dual Engine Chg.

Eng. Chg. 731200 ~0° N/A ~1 30.06.18 EGT Margin on Watch

__________________________________________________________________________________________________________________________


________________________________________________________________________________________________________________________________



9° N/A <2 31.07.18 None (EGT margin recovered)

10° 48 (CRZ) 1,8 31.08.18 None

6° N/A 1,2 30.09.18 None

17° 47 (CRZ) 1,3 31.10.18 None

18° 48 (CRZ) 1,4 30.11.18 None

5° 48 (CRZ) 1,3 31.12.18 EGT Margin on Watch

15° 46 (CRZ) 1,2 31.01.19 None

13° 46 (CRZ) 1,2 28.02.19 None

15° 45 (CRZ) 1,6 31.03.19 None

18° 46 (CRZ) 1,2 30.04.19 None

11° 49 (CRZ) <1 31.05.19 None

12° 46 (CRZ) <1 30.06.19 None

9° 46 (CRZ) <1 31.07.19 None

12° 47 (CRZ) <1 31.08.19 None

13° 44 (CRZ) <1 30.09.19 None

13° 49 (CRZ) <1 31.10.19 None

__________________________________________________________________________________________________________________________


________________________________________________________________________________________________________________________________


Reference (1 year) to show long term trend:

__________________________________________________________________________________________________________________________


________________________________________________________________________________________________________________________________



__________________________________________________________________________________________________________________________


________________________________________________________________________________________________________________________________


Condition Summary

No. 1 Engine S/N 731335 (New Purchase)

Main parameters EGT Margin 53°

Oil Pressure 46 (CRZ)

Vibrations ~1

Watch Items None

Conclusions/Recommendations None

Performed actions by previous recommendations

No. 1 Engine S/N 731200

Main parameters EGT Margin 13°

Oil Pressure 49 (CRZ)

Vibrations <1

Watch Items None

Conclusions/Recommendations None

Performed actions by previous recommendations

____________________________________________________________________________________________________________________________

EASA IE.145.073 FAA 9VOY776C

Bay 140-141, Shannon Free Zone, Shannon, Co. Clare, Ireland

Tel: +353 61 704826 Fax: +353 61 704832 E-mail: [email protected]

VIDEO BORESCOPE INSPECTION REPORT – CFM56-5A WORK ORDER: VAI-19146-E

ENGINE S/N: 731335 A/C TYPE: A320-200 CUSTOMER: KELLSTROM

MODEL #: CFM56-5A1/F A/C S/N: N/A LOCATION: TARMAC, FR

POSITION: #1 POS A/C REG: LY-VEV DATE: 8 JAN, 2019

REASON: CUSTOMER REQUEST INSPECTOR: NICK DUQUE

Page 1 of 17

VAI-E-010 (b) CFM56-5A BORESCOPE REPORT REV.01 July, 2015

LOW PRESSURE COMPRESSOR INSPECTION: Reference Aircraft MM Section 72-00-00

FAN BLADES

BLADE CONDITION:

• No major damage or defects noted.

DISPOSITION:

SERVICEABLE

LOW PRESSURE COMPRESSOR STAGE 2 (QTY 76]

BLADE CONDITION:

• Biological debris noted on several blades.

• No other major damage or defects noted.

DISPOSITION:

SERVICEABLE

mailto:[email protected]









Page 2 of 17


Low Pressure Compressor Stage 3 (QTY 76) Port S0

BLADE CONDITION:

• Biological debris noted on blades throughout

stage.


DISPOSITION:

SERVICEABLE

Low Pressure Compressor Stage 4 (QTY 76) Port S0

BLADE CONDITION:


DISPOSITION:

SERVICEABLE










Page 3 of 17


HIGH PRESSURE COMPRESSOR INSPECTION: Reference Aircraft MM Section 72-00-00

1st STAGE HPC BLADES (QTY38) Ports S1/S2

BLADE CONDITION:

• 1 blade noted with minor LE nick on tip area.

• Blades noted with minor LE erosion with minor

related nicks.


DISPOSITION:

SERVICEABLE

2ND STAGE HPC BLADES (QTY 53) Ports S2/S3

BLADE CONDITION:


DISPOSITION:

SERVICEABLE










Page 4 of 17


3RD STAGE HPC BLADES (QTY 60) Ports S3/S4

BLADE CONDITION:

• 2 blades noted with LE tip corners missing measuring 0.234” x 0.223” & 0.196” x 0.182”.

• Several blades noted with minor LE nicks & dents throughout stage.

• Blades noted with LE tip erosion.


DISPOSITION:

SERVICEABLE

Per AMM Ref. Task 72-31-00-290-001-A Sect. 1. G.

4TH STAGE HPC BLADES (QTY 68) Ports S4/S5

BLADE CONDITION:

• 1 blade noted with minor LE dent on tip area. • No other major damage or defects noted.

DISPOSITION:

SERVICEABLE










Page 5 of 17


5TH

STAGE HPC BLADES (QTY 75) Ports S5/S6

BLADE CONDITION:


DISPOSITION:

SERVICEABLE


BLADE CONDITION:

• Several blades noted with LE erosion with minor

related nicks & dents throughout stage.


DISPOSITION:

SERVICEABLE










Page 6 of 17


7TH

STAGE HPC BLADES (QTY 82) Ports S7/S8

BLADE CONDITION:

• Several blades noted with LE erosion with minor

related nicks & dents throughout stage.


DISPOSITION:

SERVICEABLE


BLADE CONDITION:

• 1 blade noted with LE nick on tip area measuring

0.030” in depth.


DISPOSITION:

SERVICEABLE

Per AMM Ref. Task 72-31-00-290-001-A

Sect. 2. F.










Page 7 of 17


9TH STAGE HPC BLADES (QTY 76) Ports S9

BLADE CONDITION:

• Several blades noted with minor LE nicks

throughout stage.


DISPOSITION:

SERVICEABLE

COMBUSTION CHAMBER Ports S10 - S15

CHAMBER CONDITION:

• Carbon accumulation noted on fuel nozzle

deflectors and sleeves.

• Minor edge erosion noted on fuel nozzle deflectors

throughout chamber.


DISPOSITION:

SERVICEABLE










Page 8 of 17


NOZZLE GUIDE VANES Ports S10 – S15

CONDITION:


DISPOSITION:

SERVICEABLE

LEFT BLANK INTENTIONALLY










Page 9 of 17


1ST STAGE HPT TURBINE BLADES (QTY 80) Ports S10 – S11/S17

BLADE CONDITION:

• 2 wear notches noted on reference blades.


DISPOSITION:

SERVICEABLE

STAGE 1 LPT VANES (QTY 162) PORTS S17,S18

CONDITION:

• No major damage or defects noted on visible

areas.

DISPOSITION:

SERVICEABLE










Page 10 of 17


LOW PRESSURE TURBINE INSPECTION: Reference Aircraft MM Section 72-00-00

1ST

STAGE LPT TURBINE BLADES (QTY 162) Ports S17,S18/S20

BLADE CONDITION:

• 1 blade noted with LE nick on midspan area (nor

area E) measuring 0.013” in depth.


DISPOSITION:

SERVICEABLE

Per AMM Ref. SUBTASK 72-54-00-290-050-A

Sect. 4.

2ND

STAGE LPT TURBINE BLADES (QTY 150) Ports S20/S21

CONDITION:


DISPOSITION:

SERVICEABLE










Page 11 of 17


3RD STAGE LPT TURBINE BLADES (QTY 150) Ports S21/S22

BLADE CONDITION:


DISPOSITION:

SERVICEABLE

4TH STAGE LPT TURBINE BLADES (QTY 134) Port S22

CONDITION:


DISPOSITION:

SERVICEABLE










Page 12 of 17


ADDITIONAL COMMENTS:

All Borescope Plugs Removed and Reinstalled By Vortex Technician: ☐ YES x NO

** HPT shrouds: No major damage or defects noted.

HPT SHROUDS










Page 13 of 17


HPC STAGE 3










Page 14 of 17


LPT STAGE 1










Page 15 of 17


HPC STAGE 3 SERVICEABLE LIMITS










Page 16 of 17


LPT STAGE 1 SERVICEABLE LIMITS










Page 17 of 17


THIS REPORT & THE ACCOMPANYING VIDEO IS SUBMITTED SUBJECT TO THE CONDITION THAT IS UNDERSTOOD & AGREED THAT THE CONTENTS ARE BASED ON DILIGENT INSPECTION & ARE EXCLUSIVE OF LATENT DEFECTS IN MATERIALS, RIGGING OR SYSTEMS NOT DETECTABLE WITHOUT REMOVAL OR DISASSEMBLY; BUT ARE BELIEVED TO BE CORRECT & ARE FAIRLY REPRESENTATIVE OF THE CONDITION OF THE ENGINE. THIS SURVEY IS SUBMITTED WITHOUT PREJUDICE & IN CONFIDENCE TO THE NAMED CLIENT & IS WITHOUT RESPONSIBILITY TO OTHERS TO WHOM IT MAY BE

SHOWN. SIGNATURE: NICK DUQUE DATE: 8 JAN, 2019


No. Component Description P/N S/N

1 ID rating Plug 390-300-241-0 YJI17949-2

2 HMU 8061-532 WYG89093

3 Main fuel Pump 714900-5 27652

4 Fuel Flow transmiter 8TJ124GGR1 GDB01358

5 Fuel/Oil Heat Exchanger 11-841193-4 YP028314-P

6 Servo Fuel Heater 45731-1251-1 FHS14829

7 Starter 3505582-45 0193-25971C

8 ECU 1518M83P19 ECDN1385

9 Lubrication Unit 336-010-004-0 25289

10 IDG Oil Cooler 930090-07 25326

12 HPTACCV 324585-5 WCPF0242C

13 LPTACCV C251490000-1 25269

14 VBV Hydraulic gear motor 396800-12 YA016559-0

15 VBV Stop Mechanism 3282970-4 26531

16 VBV Position Sensor VG11-04R 25923

17 VSV Actuator L/H 1211313-010 RK218

18 VSV Actuator R/H 1211313-010 APMME963

19 Ignition box - Upper 10-617980-1 BNDV7248

20 Ignition box - Lower 10-617980-1 BNDV5935

21 Integrated Drive Generator 740119H 4120

22 Hydraulic Pump 887673 MX606221

23 HP regulating Valve 6773E10000 01098

24 IP Check Valve 2290B020000 1074

25 Bleed Pressure regulating Valve 8774E10000 01184

26 Anti-Ice Valve 324195-1 082

27 Starter Air Valve 3290064-20 321157

28 Sensor T25 RP152-01 25188

29 Sensor T12 RP195-03 YC152566-D

ESN 731335 LRU List

LLP Status Report - MyAirTrade

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