WT339805-AV0095 PLI Report - willislease.com - (2018.09... · 03-09-2018 · SABV w/ofl : WT339805...

MINI PACK

ENGINE Model: PW127F

BUILD SPEC. 918

ESN: AV0095

TSN: 19,857.30

CSN: 21,748

TSO: 10,736.30

CSO: 10,899

TSHSI: N/A

CSHSI: N/A

RGB SN. AV0095

TSN: 19,857.30

CSN: 21,748

TSO: 10,736.30

CSO: 10,899

CONTENTS:

Engine Cert - EASA Form One with Dual FAA Release

LLP Status

Accessory Listing

Modification Log

Periodic Inspections

BSI Report

Part Certs

On-Wing Power Assurance Test

l. Approving Nrtionnl Avirtion Anthority/Country

CAA-NL - The Netherlands

2.

AUTHORISED RELEASE CERTIFICATEEASA Form I

3. I'orm Trrcking No.

ARCWTI 135'155

{.,\DDrovcd Orgnnisnlion NAm€ nnd Address

STANDARD AERO B.V.KRANENBERG 25047 TR. .. TILBURG THE NETHERLANDSStandardAero

5. \l'ork Order/('ontrrct/lnvoice:

wT339805

6. ltrm 7, Dcscriplior 8. Pnrl No. ,. Qtt 10. Scriil No I l. St{lusn\ ork

1 PW127F (8S918) TURBOPROP ENGTNE 3047600 1 AVo095 INSPECTED/TESTED

12. Remrrk

Item rndicated in block 7 has been externally post lease inspected and borescope inspected

Work performed atTSN 19857.3 / CSN 2r748. TSO 10736.3 / CSO 10899. TSHST N/A / CSHST N/A.

Complete engine has been packaged and preserved for more than 90 daysPreservation date: 21 -Aug-20'18

Ref: P&WC PWl27F (BS918) OHM 3037333 Rev. 36 and MM 3037332 Rev. 58

For additional information refer to technical documentation PCE- AV0095

Customer PO number: 872996

Additional Comments:

Note 1i lnstalled propshaft wilh S/N A0002RT5 is not affected by AD EASA,/CF2o12-12,CF-2012-12, US-2012-26-08, 5821798 Rev 5, 5821801 Rev 1, S821802 Rev 4 and5821813 Rev 3

Note 2: HP Turbine Vane Rrng Segments: Two vane segment with Calegory C damage.Requires repeat inspectron at 600 hrs interval (400 hrs f not on ECTlrr)

The work identified in block 11 and descnbed herein has been accomplished in accordance with 14 CFR Part 43 and in respect tothat work, lhe items are approved for return to seNice under Certificate no UVHY977L

I la. l'arl-lJ5-{.S0 ll.l(x\c to Scrr i.r Other reguletion sl,ecified in lllock l2

CerlifiesthatunlessolherwisespecifiedinBlockl2,theworkidentifiedinBlockllanddescribedin Block 12, was accomplished in accordance with Part-145 and in resp€ct to that work the itemsare considered ready for release lo service.

lIh.,\urhorisrrl SigIxlure

CS4474

l4c. (lcrtilicnte/Approvrl Ref. No

NL 145 1184

l4d. Nnmc

CORNE AARTS

l4e. Dntc (dd/mmm/yyyy)

03-Sep-2018

EASAFomI-l4t-hsu.lII )R I]SFR/INS I'AI I,ER ITIISPoNSIBII II IIiS. SI:E S'I A'TIiMIiNT ON 'I I IIJ ItIVIiRSIi SII)IJ

F 7 5 2-l-7 EASA Fom I (2010 09 28)

l3r, Cerlilies the iterhs idandfied ibove w.re menu[rctured ln confonnity to

I Approvert dcsign rletfl lnd Ire in I condltion for slfc opcration.

I Non-epproved design dat! specified in Block 12.

l3b. Aulhorised SignIturc Approvfl l/Aufhoritlltion Numbcr

l3d. Nsmo Dstc (dd/mInm/yyyy)

USERYINSTALLER RESPONSIBILITIES

This certificate does not automatically constitute authority to install the item(s).

Where the user/installer performs work in accordance with the regulations ofan airworthiness authority different than the airwofthiness authority sPecifed in Block l, itis essential that the user/installer ensures that his/her airworthiness authority accepts items from the airworthiness authority specified in Block 1.

Statements in Blocks l3a and l4a do not constitute installation cefiification. In allcases aircraf maintenance records must contain an installation certifcation issued in

accordance with the national regulations by the user/installer before the aircraft may be flown.

IASAfomI-145-lsu.2 F 7 5 2 I TEASAFornr I (201009 23)

StandardAero Life Limited Parts ListingCustomer : STANDARD AERO LIMITED (SAV-SAL)

Engine ModelEngine S/N

Workorder

PW127F (8S918)PC-E AVOOgs

wT339805

F 7 5.2-1-11

{2OO€ 0s 1{)

FAR 145 CRS IUVHYg77LEASA P.n 145 Nt 145 1184

RemarksAccumulatedcycles sincenew (note 1)

Life LimitCycles(note 1)

Remaining lifecycles (note 1)

Serial NumberDescrlption Part Number

lmpeller, LP

lmpeller, HP

Cover, HP Front

Disk, HP

Cover, HP Rear

Seal, lnterstage Air

Disk, LP

Disk, PT-1

Disk, PT-2

3039487

3043293

3039640

304151 1

3039639

3039172

3038412

3038513

3033914

AOOl EYAC

AOOl MNDP

A001M84K

AOOl MMM L

AOOl LWBY

TPAA6O3

A001H5A3

A001w24M

AOOO3LBB

10899

10899

12534

10899

'10899

't3624

10899

9056

21748

15000

15000

15000

15000

15000

15000

15000

30000

30000

4101

4',101

2466

4101

4101

'1376

4101

20944

8252

4101

4',101

2144

410',1

410',|

1 100

4101

20944

Note 2

Note 2

Note 2

Note 2

Note 2

Note 2

'l .'15

1

1

1.25

1

1

1

Note 2

Note 2

5282 Note 2

Note 1: Cycle data have been calculated using airworthiness limitations in the applicable maintenance manualNote 2: The P/N and S/N could not be verified since the parts were not accessed.

CS4474

Date: September-03-18 Certified: CornO Aarts Page 1 of 'l

Flight count I Nr. offactor | fliglrts

lremarnrng

Accessory Gomponent !nstallationStandardAero

Customer : STANDARD AERO LIMITED (SAV-SAL)


Workorder

F 7 5.2-1-10(20@0514)

FAR 145 CRS {t V}tY977LEASA P.n 145 Nt 1,15 1184

Governor, Prop Overspeed

Pump, Prop O/S Gov Hydraulic

Probe, NP Pulse Pickup

Sensor, Torque L-H (M)

Sensor, Torque R-H

Control Unit, Engine (EEC) (EAC)

Torque Signal Conditioner (TSc)

cH16705

cH963

19857.3

Unk

19857.3

Unk

Time Continue

Time Continue

Time Continue

Time Continue

N/A

N/A

3039242

3116499-02

31 16499-02

820154-1-002L6

N/A

Unk

Unk

34cHl 3 Unk

Unk00076910

072 Control Unil, Autofeather (AFU)

Exciter, lgnition Nr 1 (FWD)

Exciter, lgnition Nr 2 (AFT)

Harness, Elect Wiring NIain (P12,P13)

Harness, Elect Wiring (Eme0 (P20)

Harness, Elect Wiring lnsl-A (P21)

Harness, Elect Wiring lnst-B (P22)

N/R

9049400-1

9049400-1

3'l 16050-06

NN98090988

99141005

4411542

N/A

N/A

N/A

08

10

1',|

12

13

19857 3 Time Continue

Time Continue

U nk

UnknkU

985 6254 3 Time Continue

TSN TSO Work carried out this visit NotesItem Part Number Serial Number

14

15

161

Cooler. Fuel-To-Oil

Fuel Pump

Control Unit, Hydromechanical (HMU)

Control Unit, l\4echanical Fuel (MFC)

Fuel Heater

Valve, Flow Divider and Dump

Fuel Nozzle

Fuel Nozzle

Fuel Nozzle

Fuel Nozzle

'1450.0

1450 0

Time Continue

Time Continue

10845B

5009982E

N/A

3244871-8-7

't0839F

3045781-01

3045778-01

w A12429 3

Unk

9857

Lt\,15416

17

18

'1901

't902

1903

't 904

c38603V

wA22399

0413

AAA70913

PHH48O7

A17855

1VR062't 5

Unk

1114.5

Unk

Unk

Unk

Unk

Unk

Unk

Unk

Unk

Time Continue

Time Continue

Time Continue

Time Continue

Time Continue

3045778-01 Time Continue

Time Continue

463.0

463 0

463.0

463 0

CS4474Date: September-03-18

3045781-0'l

Certifiedr Corn6 Aarts Page 1 of 2

: PW127F (BS918)

: PC-E AV0095

: WT339805

Description

011

02

03

04

05

06

071

1

1

1

I

1

1

1

1

1

1

1

1

,|

,|

1

1

Accessory Gomponent lnstallationCustomer : STANDARD AERO LIMITED (SAV-SAL)


Workorder

PW127F (8S918)

PC-E qVOO95

wT339805

F 7.5 2-1-10(2008 05 r4)

FAR 145 CRS 'UVHY977LEASA Pan 145 NL 145 1184

Item Description Serial Number TSN TSO Work carried out this visit Notes

1905

1906

1907

1908

1909

1910

'191 'l

1912

1913

1914

Unk

Unk

Unk

Unk

19857.3

19857.3

19857.3

Fuel Nozzle

Fuel Nozzle

Fuel Nozzle

Fuel Nozzle

Fuel Nozzle

Fuel Nozzle

Fuel Nozzle

3045776-01

3045776-01

3045776-01

3039975

3045776-01

3045776-01

3045776-01

Unk

Unk

Unk

Unk

Unk

Unk

Time Conlinue

Time Continue

Time Continue

Time Continue

Time Continue

Time Conlinue

Time ContinueUnk

463.0

463 0

463 0

463 0

463 0

463.0

463.0

20

21

24

25

26

28

29

Unk

Unk

Unk

1

,|

1

1

,|

,l

1

1

1+2

'l+2

Fuel Nozzle

Fuel Nozzle

Fuel Nozzle

Sensor, T'l.8 Temp

Thermocouple, T6 Trim

Probe, NH Pulse Pickup (T)

Probe, NH Pulse Pickup (B)

1RV08681

1PrO4261

'l ARL'1 257

463.0

463 0

463.0

304578'l -01

3045776-0'l

3045776-01

3034652

3035968

3039242

3039242

NR02836

cH16732

cH16734

Time Conlinue

Time Continue

Time Continue

Time Continue

Time Continue

Time Continue

Time Continue

UnkNA/

Probe, NL Pulse Pickup

Valve, lC Air Bleed (HB\0

Servo Valve, HBV

Valve, P2 5 Check (Cabin Aio

lgniter Plug L-H

lgniter Plug R-H

Note 'l : Component received with engine (unless otherwise specified). TSN/TSO when available supplied by customerNote 2: Part is not installed on engine but loose in a box in engine craddle

3033509

01R31 19957-03

3118642-01

N/A

3055161-01

3055161-01

cH7826

AHXo12924

wDA't0794

Unk

Unk

Unk

Unk

Time Continue

Time Continue

Unk

Unk

Unk

Time Continue

Repaired

Time Continue

trDate: September-03-18

.11

Page2 of 2

StandardAero

lPart Number

1ARH0552

1WN06677

'tARL1254

1VF1 '1 506

1XM07605

1TP02758

1AR11273

1

1

1

,|

1

1

1

19857 3

Unk

Unk

N/A

N/A

1

1

Certifiedr Corne Aarts

F7553(ReY 32 26OcF20l0)

EASA NL I45 IIt4FAA UVHY 977 L

StandardAero Modification List

TCN: WT339E05

Part #: 3047600

Modifled to Part #:

Customer; STANDARD AERO LIMITED (SAV-SAL)

Serial#: AV0095

Model: PWl27F (BS9lE)

AIRWORTHINESS DIRECTIVES / MODIFICATIONS EMBODIED2L590 R2

27873 R3

276'1 9

UPRATE OF A PREVIOUSLY DERATED ENGINE TO ITS ORIGINALpw127F (BS918) STANDARD - FROM PW127E (BS850)** FOR ENGINES POST SB 21607: THIS SB MUST BEINCORPORATED IN CONJUNCTION WITH ATR SB ATR72_12_7O02 **PROPELLER SHAET _ I NS PECT ION

AIRVr'ORTHINESS DIRECTIVES / MODIFICATIONS FOUND EMBODIEDR3

21136271 4A

R2R3

INTERCOMPRESSOR CASE DRAIN TUBE _REPLACEMENT /MODI FlCAT lON OF** CATEGORY A COMPLIANCE FOR ENGINES WITH TUBESREWORKED PER SB 21679 R1, WHICH WERE STRESS RELIEVEDAT 1775 TO 1825 DEG F (968-996 DEG C). **** CATEGORY B COMPLIANCE FOR ENGINES WITH TUBESREWORKED PER THE ORIGINAL VERSION OE SB 21679. **lNSPECTION OE MECHANICAL_FUEL CONTROL RATIO_LEVERPREFORMED PACKlNG--STOCK REPLACEMENTPN ST3367-009, CURE DATE 4Q-06MECHANICAL EUEL CONTROL UNIT (MECU) - REPLACEMENT OFINTRODUCTION OF SPACER BETWEEN WIRING HARNESS AND P3AIR TUBEEUEL PUMP _ REPLACEMENTSHIPPING CONTAINER CAPS - REPLACEMENT OFREMOVE STEI/iART WARNER FUEL HEATER PRE-PWC SB211OOMODIEICATION OE MFCUEUEL NOZZLE _ LOCKING PLATES AND O-RINGSEUEL HEATERS (CF-zOOO-34 )

BYPASS VALVE COVER GAP INSPECTIONGAS GENERATOR CASE DRAIN PORT__ONE_TIME INSPECTIONEUEL MANIFOLD TRANSFER TUBES

271e821189

R4R1

21808 CC3278 46cE-2000-34cE-2002-3AcF-96-22us-2003-16-04us-2004-20-01us-97-17-05us-98-14-02

R3RO

RO

RO

RO

RO

RO

RO

RO

AIRWORTHINESS DIRECTIVES / MODIFIC ATIONS FOUND EMBODIED PER LOGBOOK21,419 CC3 R5

RO

R1RO

RO

R4

R4

R5

POIIER TURBINE BLADE _ REPLACEMENT OE** COMPLIANCE 3 FOR AIL PT BLADE PRIOR CONEIGURATIONSWHICH HAVE A TOTAL RUNNING TIME OF 8,OOO HOURS OR MORE **HP TURBINE SHROUD SEGMENTS - BORESCOPE INSPECTION** csPN A00035 ***NO. 18 BEARING - INSPECTION OFPROPELLER SHAFT _ INS PECT I ON(REF. PMS W101wA?21110SB)POWER TURBINE STATOR AS SEMBLY- - INS PECT IONFIRST STAGE POWER TURBINE BLADE - INSPECTION OE*** CSPN 1003455 APPLIES. EXPIRES 30 NOVEMBER 2013 ***BORESCOPE INSPECTION REDUCTION GEARBOX FIRST STAGE GEAR** CSPN 1004540 APPLIES : EXPIRES NOV. 30 2014**PROPELLER SHAFT _ REPI,ACEMENT OF** CSPN 1005865 APPLIES *+** NOTE: OPERATORS THAT COMPLIED WITH PRIOR REVISIONS OFTHIS SB MUST INCORPORATE SB 21798 R5 ,I*INSPECTION OF PROPELLER SHAFTREPLACEMENT OE PROPELLER SHAFT*** CSPN NO. 1005865 APPLY - EXPIRES NOV. 30,2Ot4 ***

27651

2769921113

271242L'7 66

2111 4

2t-198

218 0127802

R1R4

Page 1 of 2

F7553(Rev 32 264ct-2010)

EASA NL I45 I IE4FAA WHY 977 L

Modification List

TCN. WT339805 Customer: STANDARD AERO LIMITED (SAV-SAL)

Serial#: AV0095Part #: 3047600

Model: PWl27F (BS9l8)AIRWORTHINESS DIRECTIVES / MODIFICATIONS FOTJND EMBODIED PER LOGBOOK27828 R3 ENGINE FIRST STAGE POWER TURBINE BI,ADE _

INS PECT ION/ REPIACEMENT OF**cspN 1006354 AppLY- EXPIRES DEC. 31, 2018++**cspN 1007005 APPLY- EXPTRES DEC. 31, 2018**

27863 R3 FIRST STAGE POWER TURBINE BLADES -INS PECT ION,/REPLACEMENT OF** CSPN 1OO7OO5 APPLIES. EXPIRES DECEMBER 3I, 2OI8 **

CF-20O5-29 RO FIELD INSPECTION, REPLACEMENT, (AND DESTRUCTION) OEPROPELLER SHAFT

CF-2072-L2 RO PROPELLER SHAET CRACKCF-2013-02 RO EIRST STAGE POWER TURBINE BLADE FAILURE

EFFECTIVE JANUARY 37, 2473- SB21823 APPLIES.CF_94-01 RO HIGH PRESSURE TURBINE (HPT) DISKEASA/CF-2072-72 RO PROPELLER SHAFT CRACKEASA/CF-2013-02 RO EIRST STAGE POWER TURBINE BLADE FAILURE

EFFECTIVE JANUARY 31, 2013_ 5821.823 APPLIES.US-2O72-26-O8 RO PROPELLER SHAFT INSPECTION, REMOVAI & REPLACEMENT

(AMENDMENT 39_17303,.AD 2012-26-08- SUPERSEDES AD2012-t7-74)

US-2013-15_08 RO INSPECTION OE THE FIRST STAGE PT BLADES AND THEREPLACEMENT.

STANDARD AERO BVKRANENRERC 2 5047 TR TILBURCPO BOX 4I97. 5OO4 JD TILBURCTILBURO

CS447 4

Authorized Signatory

Page 2 ol2

StandardAero

Tasks carried out during shop vrsit of:

Engine S/N : PC-E AV0095 TSN : 19857.3Model & BS : PW'127F BS918 CSN:21748

DocLrmeft ldentrfer SABVOPSFT5l-13-2R6

24-May-2017

SABV Periodic lnspections and Maintenance Tasks, rer. Mainrsnanco f,ranuar chapter ofF2o.oo

SABV Wo#: WT339805 Certifying Staff : Corn6 AartsDate : 03-Sep-2018

MM 72-00-00 Salisfactory no lrndrngs x !1Reduction Gearbox (RGB)Borescope inspection

HP Vane 600 Hrs repeljtive 400 Hrs nol on ECTM tr2.Turbo-Machinery gM)Borescope inspection

MM 72-00-00INSPECTION/CHECK

HP Vane 600 HG repelitive, 400 Hrs nol on ECTM3Hot Sectionr BSI HP turbine vanes, HPT shroud segments,HP turbine blades, combustion chamber and smallexil duct


tr x4Hot Section refurbishmentDetailed HSI

MM 72-03-00INSPECTION

5.HP turbine bladesDiscard (>15000 cls / >3000 hrs)

Not disassembled

6LP turbine bladesCreep lnspection (> 4000 hrs)

crR P/N 3043515Not disassembled

Noldisassembled7First-stage power turbine blades (PT1)Drsc€rd (>10000 / 20000 / 25000 hrs)

MM 72-10,00INSPECTION/CHECK

Satlslaciory8External condition ofengine RGBVisual inspeclion of RGB for corrosion

I External condrtion of engine: front inlet caseVisual inspection of lntake and housing for corrosion


Satrslaclory

1 0External condition of engine: LP diffuser exit ductsVisual inspection

t\fl\, 72,30,00INSPECTION/CHECK Salisfacrory x tr

'| 1Exlernal condition of engine: arr bleed tnesVisual inspeclion

MM 72,01,30INSPECTION/CHECK

Satislactory x tr12.


Salislaclory xExternal condition of engine: eleclncal & ignition c€blesVisual inspection

13.MM 72-01-40INSPECTION/CHECK

N/A Post 5821562 xExternal condition of engine: HMU/MFCU (pre S821562 only)Visual inspection

x n14External condition of engine: fuel and oil linesVrsual inspeqtion

t\,l\,t 72-01-40INSPECTION/CHECK

Satislactory

Propeller shaftVisual inspeclion face H (>30000 hrs/cls)

MM 72-10.00RGB MAINTENANCE PRACTICES

Salisleclory no llndings

16.LP impellerVisuaUborescope


Salrslactory, no llndings x tr17

MM 72-00-00INSPECTION/CHECK Salislactory, nofindings x trNo 6, bearing vent transfer tube

Visual/borescope

18.iiL 72-01,50INSPECTION/CHECK

Satisfactory x trChip detectorsFunctional and operational check

19. Replaced NEW trOilfilter, mainDiscard/inspecuclean/bubble point test

i.4[r 72-01-50INSPECTION/CHECI(]SERVICING

n20Oil filter, RGB scavengeOiscardlnspecvclean/tubble point tesl

MM 72-01.50INSPECTIONiCHECI(SERVICING

Replaced NEW

CS4474

Ownerapproval M B'emans Page 1 of 2 Oualily approval S Coomans

lnspectionfTask Reference Remarks Compll6d NotChocked

X tr

tr

x trx n

trtr

X tr

StandardAero

Tasks carried out during shop visit of:

Engine S/N : PC-E AV0095 TSN : 19857.3Model & BS : PW127F 85918 CSN:21748

Document ldentfrer

lssue dale:

SABVOPSFT5l-r3,2R6

24-May-2O17

SABV Periodic lnspections and Maintenance Tasks, rer. Maintenance Manuar chapter os-2o-oo

SABV w/ofl : WT339805 certifying Staff : CornO AartsDate : 03-Sep-2018

Salisfactory n21Visual inspeclion of main oil filter by-pass indicator (mechanicalpop-out type only)

tr22Visual inspectron of scavenge filter bypass indicator (mechanicalpop-out type only)

Satrslactory

trMM 72-01-40INSPECTION/CHECK, CLEANING

Replaced NEW23.Fuelfilter HP (fuel pump)lnspecrclean and bubble pornt test

Replaced NEW24.Fuel filter, LP (fuel heate0lnspecvclean and bubble point test

MM 72-O1-40INSPECTION/CHECK CLEANING

xVrsual inspection of LP fuel filter by-pass(mechanical pop-out lype only)

tr26. TSCU (P7) and Tq sensor (P12) connectorRemove and inspect (PW123 pre S821463 only)

NILI72 01 00

x27lgniter plugs (removed from engine)Detail/visual lnspection

MM 72-01-20INSPECTIONiCHECK

LH - lnspected SalislacloryRH . hspecled Satislactory

trMM 72-01-60INSPECTION/CHECK28.

TO sensorsContinuity and resistance

nMM 72-01-60INSPECTION/CHECK

Satistactory x29.T6 systemContrnuity and resistance

Tme-Conlinued TSO 463 hours x30.Fuel nozzlesOverhaul

cMM 3056640 / 3077278

tr3 1O/S governor hydr pump relief valve replacement(4000 hours interval, pre S821570 only)

s821221

tr x32O/S governor hydr pump: bench checkPWl20A, Pl/Vl21 (85717) and PW123 series only

cMl\,1

Auto Feather Unit (AFU)lnspect and Recertity

C IVIV

CMM tr34Mechanical Fuel Control (MFCU)lnspect and Recalibrate

x35.Fuel pumplnspection for spline wear input shaft and drive gear CMM

CS4474

Ollner app.oval M. Biemans Page 2 ol 2 Qoa rty approval S Coomans

lnspection/Task Relerenco Romarks Compllod NotCh6ck6d

Xxx

Electrical tr

trx

xx

tr xx

tr

Inspection Report StandardAero WT339805_IN AV0095

NOTICE OF CONFIDENTIALITY – This document contains confidential or proprietary information. Any unauthorized disclosure, use, copying or distribution of the contents of this document or the taking of any action on the contents of this document is strictly prohibited. If received in error, please promptly return original and any copies to StandardAero.

Page 10 of 22

7. CONCLUSION

7.1 Per engine logbook entries, engine AV0095 had operated a total of 267.3 hrs and 282 flights during the last lease term.

7.2 Pre-removal Power Assurance Check [PAC] data provided showed satisfactory performance margins.

7.3 Borescope inspection revealed category C damage to HPT vane, which is acceptable for continued service provided repeat inspection at 600 hrs interval (400 hrs if not on ECTM) are carried out.

7.4 Borescope inspection confirmed that all other gas path components were in serviceable condition.

7.5 LH torque probe was changed during the last lease term.

7.6 Previous operator did not carry out preservation of oil and fuel system. A short engine run was carried out this shop visit to satisfy long term storage preservation requirements.

7.7 First life-limiter will be the HPT inter-stage air seal, with 1100 flights remaining.

7.8 At customer request, engine will be up-rated back to PW127F configuration (SB21590). Spare PW127E characterization plug is provided in engine logbook bag for possible future use.



Page 11 of 22

APPENDIX A Photographs

Figure 1: LP Impeller.

Nick in area Ca (serviceable).

Figure 2: LP Impeller.

Nick in area Ca (serviceable).



Page 12 of 22

Figure 3: HP Impeller.

Nicks in area C (serviceable).


Nicks in area C (dimension of deepest nick, serviceable).



Page 13 of 22


Minor nick in area C of Splitter Vane (serviceable).

Figure 6: Combustion Chamber Outer Liner [CCOL]. Cracks, coating loss and missing material (serviceable).



Page 14 of 22

Figure 7: Combustion Chamber Inner Liner [CCIL]. Cracks, coating loss and missing material (serviceable).

Figure 8: Small Exit Duct [SED].

Cracks in coating layer, un-bonding of coating (serviceable).



Page 15 of 22

Figure 9: HPT Vane Segment.

Airfoil leading edge burnt (category C).

Figure 10: HPT Vane Segment.

Airfoil leading edge burnt (category B).



Page 16 of 22

Figure 11: HPT Vane Segments.

Cracks on airfoil trailing edge and outer support ring (serviceable).

Figure 12: HPT Blades.

Minor coating loss leading edge (serviceable).



Page 17 of 22

Figure 13: HPT Shroud Segments. Minor rubbing marks (serviceable).

Figure 14: LPT Stator.

Small hairline cracks on leading edges (serviceable).



Page 18 of 22

Figure 15: LPT Blade.

Minor bent/deformed trailing edge (serviceable).

Figure 16: LPT Shroud Segments. Minor rubbing marks (serviceable).



Page 19 of 22

Figure 17: 1

st Stage PT Stator.

Coating loss on leading edges (serviceable).

Figure 18: 2

nd Stage PT Stator.

Hairline crack on outer shroud (serviceable).



Page 20 of 22

Figure 19: No. 6&7 Brg Transfer Tube, Vent. Minor carbon deposit on inside (serviceable).

Figure 20: Fuel & Oil Pump Drive Bevel gears.

Normal service wear (serviceable).

l. Aplrroving Nrtionrl Avi[tion Authority/Counlry

CAA-NL - The Netherlands

2.

AUTHORISED RELEASE CERTIFICATEEASA Form I

3. Form Trucking No.

ARCWTI 135'169

{. ADDroved Orgtrni$ation NAme and Addrcss

STANDARD AERO B.V.KRANENBERG 25047 TR. .. TILBURG THE NETHERLANDSStandardAero

S. \Vork Order/Contrrct/lnvoice:

wT339805

6. ltem 7. Description t, l'rrl No. 9. Qr,v 10. Scrial No, I l. Stntxsn\ ork

1 HANDLING BLEED VALVE ASSY 01R3119957-03 1 AHXO',t2924 REPAIRED

12. Remrrk

The em indicated in block 7 has been visually inspected and repaired.Work including screen aeplacement.

Work performed at TSN Unk / TSO Unk

Item has been removed from esn AV0095 TSN 18957.3 / CSN 21748

Ref.P&WC MM P/N 3037332 Rev. 58. ATA 72-01-30 Par. 5.

Customer PO number: 872996

Additional Comments

Assy consisls oflBase Unit P/N 01R3116691-02 S/N.4HX012924Servo valve P/N 31r8642-01 S/N WDA10794

The work dentifled in block 11 and descnbed herein has been accomplished in accordance with 14 CFR Part 43 and rn respect tothat work, the items are approved for return to seNice under Cert lcate no UVHY977

I laE Pirt-t{5.,,t.50 Relcrsc to scnicc Other regulAtion sperified in Block l2

Ce(ifies (hat unless orherwise specified in Block 12, the work identified in Block I I and d€scnbedrn Block 12, was accomplished in accordance with Part-145 and in respect to that work the itemsare considered ready for reletrse to service

l,lb. Allthorised Sign[ture

t,J44t 4

l4c. Cerdncrte/Approvrl Ref. No

NL 145 1184

l{d. Nnmr

CORNE AARTS

lle. Drte (dd/mmm/yyyy)

03-Sep-2018

EASA Fom l - 145 -ks0.2r,oRtlstiR/tNs'tAt.l.1iRt{tisPoNs Il.l tis.sriris'lA'lliMliNroN lliRllvlilLslisll)l:

F752-l-TEASAFom I (201009 23)

l3n. Certifics the it6ms identified rbovc w€re mxnuf[clured in conaormlty to

! lpproved dcsign d0ta rnd rrc in e condition for sifc operrtion,

! Non-npproved design d0ta specified in Block 12,

!3b. Authorised SignIture I Jc. Approvsl/AIthorisfl tlofl Numher

l3d. NBmc l3e. D{te (dd/mnm/yyyy)

WT339805-AV0095 PLI Report - willislease.com - (2018.09... · 03-09-2018 · SABV w/ofl : WT339805...

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Transcript of WT339805-AV0095 PLI Report - willislease.com - (2018.09... · 03-09-2018 · SABV w/ofl : WT339805...