borescope report w332527 - willis lease · 2018-02-09 · yaroslav sanchak, p. eng tpaf reliability...
TRANSCRIPT
MINI PACK
ENGINE Model: PW127M
BUILD SPEC. 1237
ESN: ED0569
TSN: 7,645.00
CSN: 6,919
TSO: -
CSO: -
TSHSI: -
CSHSI: -
RGB SN. ED0659
TSN: 7,645.00
CSN: 6,919
TSO: -
CSO: -
Fuel Nozzles
TSO: 540.83
CONTENTS:
Engine Cert
LLP
Accessories
Shop Inspections
Test Data
Modification List
BSI Report
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StandardAero
TCN: W332527
P/N: 3073453-01
Customer PO #: N-1013
S/N: PCE-ED0659
LIFE LIMITED PARTS LIST
Customer: TRANSPORTES AEROMAR, S.A OE C.V.
Modified to P/N:
TSN: 7645 TSO: N/A CSN: 6919 CSO: N/A
Part DescPart #lnstalled
SNlnstalled
CyclesRemCSN
COVER.HIGH PRESSURE TURBINE,RE
lnstallgd Not€s Not accessed
COVER-HIGH PRESSURE TURBINE. FR
ln3talled Notos Not accessed
DISC, POWER TURBINE 1ST
lnstallsd Notes Not accessed
OISC-HIGH PRESSURE TURBINE
lnstallod Notes Not accessed
DISC.POWER TURBINE 2ND
lnstalled Notes Not accessed
OISC-TURBINE, LOW PRESSURE
lnstallod Nolss Not accessed
HP IMPELLER
lnrtalled Notes Not accessed
LP IMPELLER
lnrtalled Notes Not accessed
SEAL AIR INTER STAGE
ln3talled Notes Not accessed
3039639
3039640
3038513
3041511
3033914
3039412
3072766-01
3072764-01
3039172
AOO3LB3 7522 747a
A0038YEA 8257 6743
A0038NPA 6919 23081
A0038884 7516 7484
A0038D0W 6919 23081
A0038M50 7522 7478
A0038K85 7551 7449
EAAC00X148 8134 6866
UAAC4lO 8965 6035
STANDARD AERO LIMITED33 ALLEN DYNE ROAD
WINNIPEG, MB R3H 1A1
CANADA
Content rs confdential and pllgieiary io StandadAerc. lnfonnalion shall noi be .eproduced or disdoced to thl.d panjes witholt the Mten cons€nt ot Stand6dAero.
Date Pdnted: February 05, 2018 10:07:14 AM Page 1 of 1
AMO# 22-58EASA.145.7059
-
StandardAero
TCN: W332527P/N: 3073453-01
Customer PO #: N-1013
S/N: PCE-ED0659
ACCESSORIES LIST
Customer: TRANSPORTES AEROMAR, S.A DE C.V.Modified to P/N:
TSN: 7645 TSO: N/A CSN: 6919 CSO: N/A
SN
E T UNIT
lnstallod Notes Functionally checled on engine testEEC
lnstalled Notgs Functionally chected on engine testEXCITER IGNITION
lnstalled Notgs Functionally checked on engine testEXCITER IGNITION
lnstallsd Notes Functionally checked on engine testFCOC
lnstallqd Notes Functionally checked on engine testFLOW OIVIDER
lnstalled Notss Functionally checked on engine testFUEL CONTROL, MECHANICAL
lnltallgd Notgs Functionally checked on engine testFUEL HEATER
lnstallqd Notes Functaonally checked on engine testFUEL PUI/lP
lnstallgd Notes Functionally checked on engine testPROBE-PULSE PICKUP
lnEtalled Notes Functionally checked on engine testPROBE.PULSE PICKUP
lnslallod Notes Functionally checled on engine testPROBE-PULSE PICKUP
lnltalled Notes Functionally checked on engine testPROBE-PULSE PICK-UP
ln3tallgd Notes Functionally checked on engine testWIRE HARNESS
lnttalled Not€s Functionally checled on engine testSENSOR TOROUE MONITOR REDUCTIO
lnstallod Notes Functionally checked on engine testSENSOR, TEMPERATURE
lnstallod Notgs Functionally checked on engine testT6 THERMO COUPLE
lnstallsd Notes Functionally checked on engine testTOROUE SENSOR
lnstall6d Notes Functionally checked on engine testVALVE-SERVO. INTERCOi/llPRESSOR 8
lnstallgd Notos Functionally checked on engine testHANDLING BLEED VALVE ASSY
lnstallod Notgs Functionally checked on engine test
12-540
1012974-4-002 12110023
9049400-1 NNA12480044
9049400-'! NNA12490056
'108458
26355-1 H0025
3244471-A c39654Y
10839F w 445719
5009982E E0033
3077761-O1 cH 1301
3077761-01 cH 1321
cH1328
3033509 cH20385
3073315-03
3073471-02
3037603 NR03778
3035968 NR05744
3116499-02 cH1445
31 18642-0'l wDA08142
3116691-02 AHX011909
STANDARD AERO LIMITED
33 ALLEN DYNE ROADWINNIPEG, MB R3H 1A1
CANADA
AMO# 22-58E4SA.145.7059
Conlenr rs confdenlial a.d prcpdetary to Sland..dAero Inlormalio. sha I .ol be reproduced o. drsdosed lo thnd pa.iies withoul the wnten co.sent oI StandadAerc
Date Printed: February 05, 2018 10:33:36 AM Paae 1 ol1
Part #
wA45383
3077761-01
EF00730
cH11'15
POST RENTAL _ LEASE FORM
TCN: W332527 ESN: PCE-ED0059
Periodic lnspections and Maintenance task ref. Maintenance Manual Chapter OS-20-OO
<,StandardAero
No lnspection Remarks Checked
1Borescope inspection of Turbomachinery and Reductiongearbox. 2138
2Borescope inspection of No. 6 & 7 bearing Vent TransferTube Assembly. PW 12O, 1 21 (BS7 2217 25\, PW'l 2 45,Pw 't27 (ElF lM) onty .
Completed 2138
Replacement of overspeed govemor hydraulic pump reliefvalve (4000 hours intemal, pre S82'1570). Not received 2138
4Bench check of Overspeed Govemor Hydraulic Pump.PW 1204, E,a.t/121 (85717) and PW123 series enginesonly. Refer to MM05-20-00 for bench check interval.
Not received 2't38
5 Chip Detector operational check Functionally checked 2138
6lnspection / replacement of main oil flter. Refer to MM05-20-00 for replacemenuinspection interval. New filter installed
7lnspection / replacement of scavenge filter. Refer toMM05-20-00 for replacemenUinspection interval. New filter installed 2't27
8Visual inspection of main oil filter by-pass indicator(mechanical pop-out type only). Completed 2138
I Visual inspection of scayenge filter by-pass indicator(mechanical pop-out type only). Completed 2't38
10lnspection / replacement of LP fuel filter. Refer to MM05-20-00 for replacemenuinspection interval. lnspected ok 2138
11lnspection / replacement of HP fuel filter. Refer to MM05-20-00 for replacemenvinspection interval. lnspected ok 2138
lnspection of Mechanical Fuel Control Completed 2138
13Visual inspection of LP fuel filter by-pass (mechanicalpop-out type only). Completed 2138
lnspection of fuel pump. 2138
'15 Overhaul of fuel nozzles. Refer to MM05-20-00 forinspection interval. Not Required 2138
to Visual inspection of electrical cables Completed 2138
17Remove, clean and inspect TSCU (P7) and torque sensor(Pl2) connector. PW123 series, pre SB2'1463 only.
N/A to model 2138
18Visual inspection of ignition system, including igniterplugs. Completed 2134
Visual inspection of extemal fuel lines Completed 2'138
20. Completed 2138
21 Resistance check of T6 system Completed 2134
22 Visual inspection of RGB extemal surfaces Completed 2134
23Visual inspection of front inlet case and rear inlet caseextemal surfaces.
Completed 2138
24 Visual inspection of diffuser exit ducts. Completed 2138
FliDate trJ I
.4-v).tul//an-:'_
Completed
3.
2',t38
12.
'14. Completed
'19.
Visual inspection of extemal oil lines.
Certified:
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AMO4 22-588ASA.145.7059
StandardAero Modification List
TCN: W332527
Part #: 3073453-01
Modified to Part #:
Customer: TRANSPORTES AEROMAR, S.A DE C.V.
Serial#: PCE-ED0659
Model: PWl27M (BS1237) ENGINE
AIRWORTHINESS DIRECTTVES / MODIFICATIONS EMBODIED21'7 98 R5 218 012tBO2 R4 27873cF-20L2-72 R0 EASA/CF-2012-12
R1R3RO
AIRWORTHINESS DIRECTIVES / MODIFICATIONS FOUND EMBODIED PER LOGBOOK21803 R5 2L854 R12786I R2 CF-2014-47 R0EASA,/CF-2o14-41 RO
STANDARD AERO LIMTTED33 ALLEN DYNE ROADWINNTPEC, MB R]H IAICANADA
Authorized Signatory 0h,u-t-FEB 3 5 20t8
Page 1 of 1
TurboProp Programs, Airlines and Fleets Sector
1
33 Allen Dyne Road Winnipeg, Manitoba Canada R3H 1A1
Borescope Report W332527
Borescope and Visual Inspection
Of
Turbomachinery and Reduction Gearbox
Engine Model PC-E ED0659 RGB ED0659
Prepared for: Transportes Aeromar, S.A. De C.V. Attn: Mr. Erubiel Cruz Gallardo Prepared by: _______________________________ Yaroslav Sanchak, P. Eng TPAF Reliability Engineer Reviewed by: ________________________________ Krista Thoroski Customer Account Leader Date: January 30, 2018
TurboProp Programs, Airlines and Fleets Sector
2
Distribution List
Name Company
Mr. Erubiel Cruz Gallardo Transportes Aeromar, S. A De C. V.
Lisa Munoz
Senior Warranty Leader
Turboprop Programs, Airlines & Fleets Sector, StandardAero Winnipeg
Krista Thoroski
Customer Account Leader
Turboprop Programs, Airlines & Fleets Sector, StandardAero Winnipeg
TurboProp Programs, Airlines and Fleets Sector
3
1. Introduction The engine PW127M (BS 1237) S/N: ED0659 was borescope inspected and evaluated Pratt & Whitney Canada
Maintenance Manual 3037332.
2. Engine History
Turbomachinery S/N: ED0659 Reduction Gearbox S/N: ED0659
TSN : 7645.0 hours TSN : 7645.0 hours
CSN : 6919 CSN : 6919
TSO : N/A TSO : N/A
CSO : N/A CSO : N/A
3. Borescope Inspection Findings and Required Action
Inspection Point
Recurring Inspection Req’d Findings:
Yes No Hours
RGB Input & Helical Gears
RGB Pinion Gears
RGB Bullgear
LP Impeller Minor nicks. Repaired in-situ. Acceptable.
HP Impeller
IC Case
Outer CC Liner Coating and cooling ring coating and base material cracking and erosion. Acceptable.
Inner CC Liner Coating and cooling ring coating and base material cracking and erosion. Acceptable.
Small Exit Duct
HPT Blades
HPT Vane Segments 1500/1000* Trailing edge cracks and hairline cracks in inner shroud. Category A damage.
HPT Shroud Segments Minor rubs. Acceptable.
LPT Blades Light tip rubs. Acceptable.
LPT Shroud Segments Light rubs. Acceptable.
LPT Stator LE cracking. Acceptable.
PT1 Stator
PT1 Blades
PT2 Blades
PT2 Stator
Fuel & Oil Pump Gears
Accy Drive Bevel Gears
Starter Generator Gear
No. 6&7 Brg Vent Tube
No. 5 Bearing Cavity
4. Additional Findings / Observations/ Comments
*Reference to HPT vanes found condition: For engine on ECTM: 1500 FH max and for engine not on ECTM: 1000 FH max.
TurboProp Programs, Airlines and Fleets Sector
4
5. Photographs
Input Shaft
1st Stage Helical Gears
TurboProp Programs, Airlines and Fleets Sector
5
2nd Stage Pinion Gears
2nd Stage Reduction Gear (Bullgear)
AGB Gears
TurboProp Programs, Airlines and Fleets Sector
6
LP Impeller
HP Impeller
No. 5 Bearing Cavity
TurboProp Programs, Airlines and Fleets Sector
7
Towershaft Gears
IC Case
Combustion Chamber Liners
TurboProp Programs, Airlines and Fleets Sector
8
Small Exit Duct
HPT Vane Ring Segments
HPT Blades
TurboProp Programs, Airlines and Fleets Sector
9
LPT Stator
LPT Blades
PT1 Stator
TurboProp Programs, Airlines and Fleets Sector
10
PT1 Blades
PT2 Blades
PT2 Stator
TurboProp Programs, Airlines and Fleets Sector
11
No.6 & 7 bearing vent tube