Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

In House Capability List APU GTCP85-SERIES GMF AeroAsia NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

1

TRP/49-21/001

TURBINE NOZZLE SPACER

3600640-1

49-21-73

(1)

Repair turbine spacer by machining

(1)

Repair cracks item 1 and 3

(2)

Repair cracks item 2

(3)

Repair/replace damaged item 4

(4)

Repair damaged insulator strips item 6

(5)

Repair cracks item 5

(1)

(3)

Repair crack in weld seam (item 1). Repair crack in welded seam and adjoining material (item 2) and crack in intersecting weld seam (item 3) Heat Treatment

(4)

NDT

(1)

Repair damaged cracks.

(2)

Replace damaged/loose nut plates.

2

3

4

TRP/49-21/002

TRP/49-21/003

TRP/49-21/004

COMPRESSOR INLET PLENUM ASSEMBLY

TURBINE PLENUM ASSEMBLY

TAILPIPE ASSEMBLY

3600729-1

3600734-1

3601618-1

49-21-73

49-21-73

49-21-73

(2)

(1)

5

TRP/49-21/005

SEGMENTED TURBINE NOZZLE

Prepared by: Mohammad Andito / 532006

3601669-1/-2/-7/8/-13/-14/-15/-16

(2) 49-21-73

(3)(4)

DESCRIPTION

Repair damaged cracks. Repair erosion and corrosion damage. Repair damaged coating.

(5)

The segmented turbine nozzle airfoils can be repaired

(6

Strip Aluminide coating and recoat with Platinum aluminide. Page 1 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

6

7

CAPABILITY LIST NO.

TRP/49-21/006

TRP/49-21/007

PART NAME

COMPRESSOR INLET PLENUM ASSEMBLY

TAILPIPE ASSEMBLY

PART NUMBER

3602652-1/-2

3602953-1/-2

ATA REFERENCE

49-21-73

49-21-73

REPAIR SCHEME (1)

Repair damaged cracks item 1 and 3.

(2)

Repair cracks in welded seam and adjoining metal.

(3)

Repair/Replace damaged nut plates (Item 4).

(4)

Repair/Replace damaged or loose insulator strip (Item 6)

(5)

Weld loose brackets (Item 5)

(1)(a)(b)(c)

Replace loose or damaged nut plates.

(1)

Repair loose or damaged Inserts.

(2)

Repair damaged Vane.

(6)

TRP/49-21/008

FIRST STAGE DIFFUSER

3603288-1/-2

49-21-73

Rework Surfaces A

(7)(b)(2)

Rework Surfaces C Rework Diameter AC by Metal Spray.

(8)(b)(2)

Rework Diameter DC by Metal Spray.

(10)

(1) (2) TURBINE NOZZLE AIRSEAL

3603350-1/-2/-3/4

49-21-73

(3) (4) (5)

Prepared by: Mohammad Andito / 532006

Rework Diameter AC and DC

(8)(b)(1) (9)

TRP/49-21/009

Replace damaged steel vane tips Rework Surfaces A and C.

(7)(b)(1) (8)(a)

9

Weld repair cracks.

(2)

(7)(a) 8

DESCRIPTION

Repair the vane tips by weld repair to remove erosion Repair the fretting and/or corrosion damage to the port flange surfaces Repair fretted damage from trailing edge of vanes. Repair erosion damage of vane leading edge is less than oneeight inch deep. Repair scoring that is less than 0.030 inch deep on shroud. Repair scoring that is more than 0.030 inch deep but less than 0.060 inch depth. Repair damaged worn stud.

Page 2 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (6) (7) (8)

10

11

TRP/49-21/010

TRP/49-21/011

TURBINE NOZZLE SPACER

MATCHED HOUSING ASSEMBLY SET

Prepared by: Mohammad Andito / 532006

3603510-1

3603708-1/-2/-3/5/-6/-7/-8

49-21-73

49-21-73

(1)

DESCRIPTION Repair Aluminize areas of turbine nozzle vanes. Repair vanes for erosion, sulfidation and burn damage (REPAIR OUTSIDE) Repair vane by stripping and re-coating with silicone-modified aluminide. Repair turbine spacer by machining

(1)

Repair damaged magnesium surfaces.

(2)

Repair anodized aluminum parts.

(3) (4)

Repair chipped, scratched or damaged painted or primed surfaces Prepare parts for repainting exterior surfaces only.

(5)

Replace studs and inserts.

(6)

Repair steel parts.

(7)

Replace loose, worn or damaged bushings.

(8) (8A)

Replace Bushing (30 through 80 and 180 through 240) Repair Oversized Bores

(9)

Repair Diameter FE and/or A to get dimensional limits

(10)

Repair minor damage to Surface BB.

(11)

Weld repair the gearbox and input housing

(12) (13)

Repair alignment pin bores or replace Alignment Pin Bushings Part No. 693472-11 Repair cracked lug for hole number 7.

(14)

Replace nozzle and stud assembly if inspection shows damage

(15)

Repair the oil jet bore by installation of a threaded sleeve

(16)

Repair idler spur gearshaft boss, Centerline VII

(17)

Repair gouging and scoring to accessory mount bores

(18)

Repair 2.8745 to 2,8755 inch Diameter E by application of Metal Spray. Page 3 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (19) (20) (21)

(23) (24)

Parent metal bore repair in mount pad (REPAIR OUTSIDE)

(25)

Remove and replace bearing liners with oversize bearing liners on CL1, CL2, CL3, CL4, CL5, CL6, CL8 and CL9 (REPAIR OUTSIDE) Weld repair of cracks in gearbox housing and locating pin bore (REPAIR OUTSIDE) A proprietary repair is available for the housing assembly and locating pin bore providing all other limits in check procedures are met (REPAIR OUTSIDE) Sleeve repair parent metal bore Diameters CL1, CL2, CL3, CL4, CL5, CL6, CL7, CL8, CL9 and CL10 (REPAIR OUTSIDE)

(26) (26) (27)

(1) (2) (3) TRP/49-21/012

COMBUSTION CHAMBER LINER ASSEMBLY

3603841-1

49-21-73

Repair cracks Repair metal thinning from corrosion or erosion and deformation. Replace cap assembly.

(4)

Replace damaged deflector.

(5)

Replace damaged cooling skirts

(6)

Replace damaged discharge ring

(7)

Replace damaged spacers

(8)

Replace floating grommet Apply thermal barrier coating to the inside surface of the combustor

(9)

Prepared by: Mohammad Andito / 532006

Plug repair damaged threads (9/16-18UNJF-3B) at AN-6 Oil Port on thin half of gearbox housing. Metal spray repair Surface BB. Replace fitting bores alignment bushings with oversize bushings. Repair of damaged threaded holes in mounting pads (REPAIR OUTSIDE) Repair of oil passage to Centerline 1(REPAIR OUTSIDE)

(22)

12

DESCRIPTION

Page 4 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

13

CAPABILITY LIST NO.

TRP/49-21/013

PART NAME

ACCESSORY DRIVE HOUSING ASSEMBLY

PART NUMBER

3604090-1

ATA REFERENCE

49-21-73

14

TRP/49-21/014

TURBINE PLENUM ASSEMBLY

3604213-1/-2

49-21-73

15

TRP/49-21/015

TAILPIPE (EXHAUST DUCT) ASSEMBLY

3604498-1

49-21-73

REPAIR SCHEME (1)

Replace bushing in case assembly

(2)

Replace housing in case assembly

(3)

Install sleeves and repair boss on fan drive shaft bore

(4)

Repair damaged oil pump shaft seal bore

(5)

Machine oil sump for oil drain slot.

(6)

Replace jet.

(1)

Repair crack in weld seam (item 1). Repair crack in welded seam and adjoining material (Item 2) and crack in intersecting welded seam (Item 3) by patching

(2)

(1)(a)(b)(c)

Repair shaft assembly

(2)

(4)

Replace shaft assembly (Part No. 3604604-1/-3) Repair turbine wheel blade trailing edge damage (Part No. 3604604-2) Repair turbine wheel blade trailing edge damage Repair turbine wheel saddle area damage

(5)

Repair turbine wheel blade tip cracking and erosion damage

(6)

Repair turbine wheel blade tip impact damage

(7)

(11)

Repair turbine wheel blade leading edge minor damage Repair turbine wheel blade leading edge damage if beyond step (7) limits Repair turbine wheel blade contour, Surface G, damage Balance wheel and shaft assembly. Refer to SPM, Method 412A, 412C Repair internal diameter of shaft to salvage part.

(12)

Repair outside Dimensions of salvaged shaft

(3A)

16

TRP/49-21/016

3604604-1/-2/-3

49-21-73

(8) (9) (10)

Prepared by: Mohammad Andito / 532006

Weld repair cracks.

(1) (3)

WHEEL AND SHAFT ASSEMBLY

DESCRIPTION

Page 5 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

17

CAPABILITY LIST NO.

PART NAME

TRP/49-21/017

COMBUSTOR CAP ASSEMBLY

PART NUMBER

3604991-1

ATA REFERENCE 49-21-73

18

TRP/49-21/018

MULTISPEED SWITCH GEARSHAFT ASSEMBLY

3605244-1

49-21-73

19

TRP/49-21/019

FUEL CONTROL DRIVE GEARSHAFT ASSEMBLY

3605245-1

49-21-73

REPAIR SCHEME (1)

Cold straighten combustor cap assembly

(2)

Weld repair cracks in combustor cap assembly

(3)

Repair combustor cap assembly atomizer mounting surface.

(1)

Repair Diameter A or B

(2)

Replace damaged splined end coupling.

(1)

Repair loose plug in gearshaft

(2)

Repair Diameters A, B or C if inspection shows damage

(3)

Replace damaged splined end coupling.

(1)

(3)

Repair cracks Repair metal thinning from corrosion or erosion and deformation. Replace cap assembly.

(4)

Replace damaged swirl.

(5)

Replace damaged cooling skirts

(6)

Replace damaged discharge ring

(7)

Replace damaged spacers

(8)

Replace floating grommet

(9)

Replace damaged tube assembly Apply thermal barrier coating to the inside surface of the combustor

(2)

20

TRP/49-21/020

COMBUSTION CHAMBER LINER ASSEMBLY

3605384-3/-4/-7/8

49-21-73

(10)

(1)

(3)

Repair cracks Repair metal thinning from corrosion or erosion and deformation. Replace cap assembly.

(4)

Replace damaged cooling skirts

(5)

Replace damaged discharge ring

(2) 21

TRP/49-21/021

COMBUSTION CHAMBER LINER ASSEMBLY

Prepared by: Mohammad Andito / 532006

3606723-3/-4/-7/8

49-21-73

DESCRIPTION

Page 6 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (7)

Replace damaged spacers

(8)

Replace floating grommet Apply thermal barrier coating to the inside surface of the combustor

(9)

22

TRP/49-21/022

WHEEL AND SHAFT ASSEMBLY

3606982-1

49-21-73

(1)

Repair shaft assembly

(2)

Replace shaft assembly

(3)

Repair turbine wheel blade trailing edge damage

(4)

Repair turbine wheel saddle area damage

(5)

Repair turbine wheel blade tip cracks and erosion damage

(6)

Repair turbine wheel blade tip impact damage

(7)

(11)

Repair turbine wheel blade leading edge minor damage Repair turbine wheel blade leading edge damage if beyond step (7) limits Repair turbine wheel blade contour, Surface G, damage Balance wheel and shaft assembly. Refer to SPM, Method 412A, 412C Repair internal diameter of shaft to salvage part.

(12)

Repair outside Dimensions of salvaged shaft

(1)

Repair weld cracks in tube wall

(2)

Repair weld circumferential cracks in radius of flange

(3)

Repair cracked weld or brazed joint in Area A

(4) (5)

Repair threads in bolt holes that are damaged beyond chasing, tapping and/or suitable insert installation. Repair oversize thread in forward flange

(6)

Replace threaded flange

(7)

(Part No. 3607748-1) Machine exhaust duct to allow clearance on assembly between duct and adjacent torus.

(8) (9) (10)

23

TRP/49-21/023

EXHAUST PIPE ASSEMBLY

Prepared by: Mohammad Andito / 532006

3607748-1

49-21-73

DESCRIPTION

Page 7 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

24

CAPABILITY LIST NO.

TRP/49-21/024

PART NAME

TURBINE TORUS ASSEMBLY

PART NUMBER

3607850-4/-6

ATA REFERENCE

49-21-73

REPAIR SCHEME

DESCRIPTION

(1)(a)

Repair cracked torus skin

(1)(b)

Repair cracks in seam weld

(2)

Repair cracked forged ring

(3)

Repair damaged torus skin

(3A)

Alternate method of weld flush patch repair

(4)

Replace damaged inlet flange

(5)

Replace damaged inlet flange

(6)

Replace damaged studs

(7)

Replace damaged ring and shield assembly

(8)

Replace damaged ramp

25

TRP/49-21/025

REAR TURBINE SEAL

3609143-1/-2/-3/4

49-21-73

(1)

Repair housing by kiss grinding

26

TRP/49-21/026

REAR TURBINE SEAL

3609219-1/-2

49-21-73

(1)

Repair housing by kiss grinding

(1)

Repair fretting and erosion to Diameter B and brackets.

(2)

Repair dents and cracks in heat shield.

(3)

Repair damaged brackets or weld cracks

(4)

Replace damaged to missing brackets.

27

TRP/49-21/027

HEAT SHIELD

3609467-1

49-21-73

Perform NDT after repair process.

28

TRP/49-21/028

TURBINE WHEEL SHROUD

Prepared by: Mohammad Andito / 532006

3611904-1

49-21-73

(1)

Repair damaged Diameter E

(2)

Repair damaged Surface M and Dimension N

(3)

Repair damaged Diameters C

(3a)

Repair wear or damage on Diameter B

(4)

Repair damaged Surface T

(5)

Repair damaged Surface M and Dim. X Page 8 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (6)

Repair damaged cracks on Surface H

(7)

Repair damaged Surface H with abrasive cloth

(8)

Repair damaged Surface H by Machine

(9)

Repair damaged threads

(10)

Repair damaged Surface M is more than 0.015 inch

(11)

Repair damaged Surface H per figure 602

(1)

(3)

Repair cracks Repair metal thinning due to corrosion or erosion and deformation Replace cap assembly

(4)

Replace damaged deflector.

(5)

Replace damaged cooling skirts

(6)

Replace damaged discharge ring

(7)

Replace damaged spacers

(8)

(Part No. 3603723-3/-6) Replace floating grommet Apply thermal barrier coating to the inside surface of the combustor

(2)

29

TRP/49-21/029

COMBUSTION CHAMBER LINER ASSEMBLY

369597-VARIOUS

49-21-73

(9)

(1) (2)

30

TRP/49-21/030

COMBUSTION CHAMBER LINER ASSEMBLY

Prepared by: Mohammad Andito / 532006

369937-30/-40

49-21-73

DESCRIPTION

Repair cracks Repair metal thinning due to corrosion or erosion and deformation

(3)

Replace cap assembly

(4)

Replace damaged deflector.

(5)

Replace damaged cooling skirts

(6)

Replace damaged discharge ring

(7)

Replace damaged spacers

(8)

(Part No. 369937-30/-40) Replace floating grommet

Page 9 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

31

CAPABILITY LIST NO.

TRP/49-21/031

PART NAME

INTERSTAGE AIR DUCTS

PART NUMBER

372696

ATA REFERENCE

49-21-73

REPAIR SCHEME (1)

Weld repair mount lugs

(2)

Repair corrosion damage to Surface V

(3)

Lap mating surfaces

(1)(k)

32

33

TRP/49-21/032

TRP/49-21/033

FAN DRIVE SHAFT ASSEMBLY

ACCESSORY CASE ASSEMBLY

372822-2

372896-16/-19/-20

49-21-73

49-21-73

34

TRP/49-21/034

TURBINE NOZZLE BOLT SPACER

373685

49-21-73

35

TRP/49-21/035

PLANET GEAR CARRIER ASSEMBLY

378916

49-21-73

36

TRP/49-21/036

FAN AIR INLET PLENUM ASSEMBLY

379264

49-21-73

Prepared by: Mohammad Andito / 532006

DESCRIPTION

Reprotect / Touch up the surface

(1)

Replace worn jaw and/or rotor.

(2)

Repair fan drive shaft bearing diameters.

(1)

Replace bushing in case assembly.

(2)

Replace housing in case assembly.

(3)

Install sleeves and repair boss of fan drive shaft bore

(4)

Repair damaged oil pump shaft seal bore.

(5)

Machine oil sump for oil drain slot.

(6)

Replace jet

(7)

(Part No. 372896-16/-19) Install replacement spacer.

(8)

(Part No. 372896-16/-19) Install replacement guard.

(1)

Repair turbine spacer

(1)

Replace defective inserts

(2)

Repair planet gear carrier

(1)

Repair cracks (item 1 and 3)

(2)

Repair cracks in welded seam and adjoining material (item 2)

(3)

Repair/Remove damaged nutplates (item 4)

Page 10 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

37

TRP/49-21/037

OIL AND BREATHER FITTING

379484

49-21-73

(1)

Repair fretting on cast surface

(1)

Remove fretting from trailing edge of vanes

(2)

Repair erosion of vanes leading edge

(3)

Repair scoring that is less than 0.030 inch deep on shroud Machine out cracks and scoring that are less than 0.060 inch in depth on shroud Repair damaged or worn stud

(4) 38

TRP/49-21/038

TURBINE NOZZLE

379509/-4/-6/-16/22

(5) 49-21-73

(6) (7) (8) (9) -

NO

CAPABILITY LIST NO.

PART NAME

Prepared by: Mohammad Andito / 532006

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

DESCRIPTION

Aluminize repaired areas of turbine nozzle vanes Repair of vanes for erosion, sulfidation and burning damage (REPAIR OUTSIDE) Replace vanes with burnt or cracked trailing edge and with leading edge erosion and shroud cracks (REPAIR OUTSIDE) Strip and recoat with silicone-modified aluminide. Repair damaged Vanes more than Repair (1) (2) by weld.

DESCRIPTION Page 11 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

39

CAPABILITY LIST NO.

TRP/49-21/039

PART NAME

STAGE DIFFUSER HOUSING ASSEMBLY

PART NUMBER

379515/-30

ATA REFERENCE

49-21-73

REPAIR SCHEME (1)

Replace damaged or loose inserts and studs

(2)

If examination revealed corrosion in O-ring groove (Detail A)

(2A)

Repair O-ring groove if corrosion is more than machining limits

(2B)

Repair Diameter P

(3)

Repair Surface FF

(4)(a)

Repair Surface DD

(4)(b) (5) (5A) (6)

Repair Surface DD by Metal Spray Repair Surface HH Repair Surface HH using metal spray Repair surface SS

(6A)

Repair surface SS using metal spray

(7)(a)

Repair Surface AA

(7)(b)

Repair Surface AA using metal spray

(8)

Repair Corrosion damage

(8A)

Repair Heavy Corrosion damage

(12)

(Recommended Method) Replace shroud contour

(13)

(Alternate Method 1) Replace shroud contour

(14)

(Alternate Method 2) Replace shroud contour

(14A)

(Alternate Method 3) Replace shroud contour

(15)

(16)

Repair cracks or stripped threads in mounting pads (Part No. 379515 only and repaired Part No. 379515-T24657) Repair cracks next to mount pads. Repair stripped or damaged threads in housing assembly

(17)

Repair Diameter Q with metal spray

(18)

Sleeve corroded

(15A)

(18A)

(Alternate Method) Sleeve corroded

(19)

Repair Surface FF by installing ring

(20)

Repair damaged coating. Repair Thread Hole Blow out per SB GTCP85-49-7638 (REPAIR IN HOUSE)

(21)

Prepared by: Mohammad Andito / 532006

DESCRIPTION

Page 12 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

(1)(a)

Repair Surface F

(1)(b)

To repair major rubs

(1A)

Repair Diameter A

(2)

40

TRP/49-21/040

INTERSTAGE HOUSING ASSEMBLY

379518

49-21-73

Surface E can be reworked to establish parallelism

(3)(b)

(6)(a)

Surface E by Metal Spray Repair pitting and other corrosion damage on duct mounting flanges Repair Surface F by replace shroud contour Repair damage on Diameter B, see Sheet 1, is more than metal spray limits, step (2) Repair Diameter C

(6)(b)

Repair Diameter C by Metal Spray

(6)©

Repair Diameter C by Sleeve

(3A)

(5)

(7)

Repair damaged coating.

(1)

Repair loose or damaged Inserts.

(2)

Repair damaged Vane.

(6)

Rework diffuser to incorporate steel vanes

(7)(a) TRP/49-21/041

FIRST STAGE DIFFUSER

379520

49-21-73

Rework Surfaces A and C.

(7)(b)(1)

Rework Surfaces A

(7)(b)(2)

Rework Surfaces C

(8)(a)

Rework Diameter AC and DC

(8)(b)(1)

Rework Diameter AC by Metal Spray.

(8)(b)(2)

Rework Diameter DC by Metal Spray.

(9) (10)

Prepared by: Mohammad Andito / 532006

Repair Diameter B

(3)(a)

(4)

41

DESCRIPTION

Repair the vane tips by weld repair to remove erosion Repair the fretting and/or corrosion damage to the port flange surfaces

Page 13 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (1)(3)(4) (2)(3)(4)

42

TRP/49-21/042

PLENUM ASSEMBLY

379528/-2/-3

49-21-73

(5) (6) (7)

43

44

45

TRP/49-21/043

TRP/49-21/044

TRP/49-21/045

EXHAUST PIPE ASSEMBLY

OIL BREATHER TUBE

FIRST STAGE IMPELLER

379529

379531-1

379547

49-21-73

49-21-73

49-21-73

Repair crack in weld seams (item 1) Repair crack in welded seam and adjoining material (item 2) and crack in intersecting welded seams (item 3) by patching Repair Surface A flatness Repair plenum flange GTAW weld repair turbine plenum assembly. Refer to Standard Practices Manual (SPM) 20-00-02/70-00-01, Method 411C

(1)

Repair weld cracks in tube wall

(2)

Repair weld circumferential cracks in radius of flange

(3)

(5)

Repair cracked weld or brazed joint in Area A Repair threads in bolt holes that are damaged beyond chasing, tapping and/or suitable insert installation. Repair oversize thread in forward flange

(6)

Replace threaded flange

(1)

Repair Diameter A

(4)

(1)

Straighten repair of bent blade condition.

(2)

Remove nicks, dents, rubs, or other blade damage.

(3)

Hand finish repair of raised material in curvic tooth surface.

(4)

Machine Diameter B to remove damage.

(5)

Balance the impeller.

(6)

(8)

Shot peen the impeller. Weld repair of blade leading edge and contour (REPAIR OUTSIDE) Grind repair of curvic (REPAIR OUTSIDE)

(9)

Weld repair of curvic (REPAIR OUTSIDE)

(7)

Prepared by: Mohammad Andito / 532006

DESCRIPTION

(10)

Weld repair Diameter D and/or Surface F (REPAIR OUTSIDE)

(11)

Replace curvic coupling and barrel (REPAIR OUTSIDE) Page 14 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (1)

Straighten repair of blades bent condition.

(2)

(4)

Remove nicks, dents, rubs, or other blade damage. Hand finish repair of nicks, dents or vibroscribe markings from backface. Hand finish repair of raised material in curvic tooth surface

(5)

Machine Diameter D to remove damage.

(6)

(10)

Metal spray repair Diameters B, C and/or D, Fig. 601 (Sheet 6). Balance the impeller. Refer to SPM 20-00-02/70-00-01, Method 412B. Shot peen the impeller. Weld repair of blade leading edge and contour (REPAIR OUTSIDE) Grind repair of curvic (REPAIR OUTSIDE)

(11)

Weld repair of curvic (REPAIR OUTSIDE)

(12)

Weld repair Diameters B, C and/or Surface A (REPAIR OUTSIDE)

(13)

Replace curvic coupling and barrel (REPAIR OUTSIDE)

(3)

46

TRP/49-21/046

SECOND STAGE COMPRESSOR ROTOR

379548-50

49-21-73

DESCRIPTION

(7) (8) (9)

47

TRP/49-21/047

IDLER GEARSHAFT

379557

49-21-73

(1)

Repair Diameter A

48

TRP/49-21/048

BEARING RETAINER

379561

49-21-73

(1)

Repair Diameter A if inspection reveals damage

49

TRP/49-21/049

HIGH SPEED PINION GEAR

379564

49-21-73

(1)

Repair Diameter A or B if inspection reveals damage

50

TRP/49-21/050

IDLER GEAR ASSEMBLY

379604

49-21-73

(1)

Repair Diameter A or B if inspection reveals damage

(1)

Repair loose plug in gearshaft

51

TRP/49-21/051

FUEL CONTROL DRIVE GEARSHAFT ASSEMBLY

379605

49-21-73

(2)

Repair Diameter A, B or C if examination shows damage

(3)

Replace fuel control drive gearshaft assembly splined

Prepared by: Mohammad Andito / 532006

Page 15 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

52

CAPABILITY LIST NO.

PART NAME

TRP/49-21/052

MULTISPEED SWITCH GEARSHAFT ASSEMBLY

PART NUMBER

379606

ATA REFERENCE

49-21-73

53

TRP/49-21/053

FAN IDLER SPUR GEAR

379607

49-21-73

54

TRP/49-21/054

OIL PUMP DRIVE GEARSHAFT ASSEMBLY

379608-1

49-21-73

55

TRP/49-21/055

STARTER DRIVE CLUSTER GEAR

379609

49-21-73

56

TRP/49-21/056

OUTPUT DRIVE GEARSHAFT

379610

49-21-73

REPAIR SCHEME

(1)

Repair loose plug in gearshaft

(2)

Repair Diameter A or B if examination shows damage

(3)

Replace multispeed switch gearshaft assembly splined end

(1)

Repair Diameter A or B if inspection reveals damage

(1)

Repair loose plug in gearshaft

(2)

Repair Diameter A or B if inspection reveals damage

(1)

Repair Diameter A or B if inspection reveals damage

(1)

Repair loose plug from gearshaft assembly.

(2)

Repair Diameter A or B if examination shows damage

(3)

Balance output drive gearshaft assembly. Repair chipped, cracked, broken or worn spline teeth (REPAIR OUTSIDE) Output drive gearshaft assembly gear teeth that are chipped no more than the limits of Dimension AF and/or AG

(4) (5)

57

58

TRP/49-21/057

TRP/49-21/058

IDLER SPUR GEAR

COMPRESSOR INLET PLENUM ASSEMBLY

Prepared by: Mohammad Andito / 532006

379615

379666

49-21-73

49-21-73

DESCRIPTION

(1)

Repair Diameter A if inspection reveals damage

(1)

Repair cracks (Items I and 2) by patching

(2)

Repair crack (item 3)

(3)

Remove damaged nut plates (item 4).

(4)

Replace damaged or loose insulator strip (item 5)

Page 16 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

59

TRP/49-21/059

EXHAUST DUCT FLANGE ASSEMBLY

379692-20

49-21-73

(1)

TRP/49-21/060

INLET ASSEMBLY

379713/-1

49-21-73

(1)(a)

Repair Surface F. Repair Surface F by Metal Spray.

(2)

Repair Diameter A to get dimensional limits

(3)

Repair Diameter Q

(4)(a)

Rework Surface C to limit of Dimension J

(4)(b)

Rework Surface C to limit of Dimension J by Metal Spray Repair/Rework Diameter B

(6)(b)

Repair/Rework Diameter B by Metal Spray

62

TRP/49-21/062

TURBINE WHEEL SHROUD

EXHAUST DUCT FLANGE ASSEMBLY

Prepared by: Mohammad Andito / 532006

379727-1/-2

379775-1/-461

49-21-73

49-21-73

Repair/Rework Diameter B by fabricate sleeve

(7)

Repair Diameter Q to dimensional limits.

(8)

(10)

Rework Diameter GA. See Sheets 10 through 13. Repair Diameter A, if damaged beyond metal spray limits, by installing a sleeve Repair damaged coating.

(1)

Repair Diameter A

(1)(d)

Repair Diameter B

(1)(e)

Repair damaged bolt holes

(1)(f)

Vane erosion damaged

(9)

TRP/49-21/061

Repair Surface F by fabricate sleeve.

(6)(a) (6)©

61

Weld repair cracks

(1)(b)

(5) 60

DESCRIPTION

(1)

Weld repair cracks

(2)

Replace loose or damaged nut plates.

Page 17 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (1) (1)©

63

TRP/49-21/063

TURBINE TORUS ASSEMBLY

379794

49-21-73

TRP/49-21/064

SECOND STAGE DIFFUSER

379801/-20

49-21-73

(3)

Repair damaged torus skin

(4)

Replace damaged inlet flange Part No. 3602679-1

SECOND STAGE COMPRESSOR ROTOR

Replace damaged studs

(6)

Replace damaged ring and shield assembly

(7)

Replace damaged cover assembly

(1)

Remove and replace cracked, bent or worn diffuser plate

(2)

If erosion of Surface E is more than the allowable limits

(3)

Repair damage to Diameter B

(4)

Repair damage to Diameters C and/or D

(5)

Repair damage to Surface F

(6)

Repair damaged vane leading edges

(1)

Straighten repair of bent blade condition.

(2)

Remove nicks, dents, rubs, or other blade damage. Hand finish repair of nicks, dents or vibroscribe markings from backface. Hand finish repair of raised material in curvic tooth surface.

(5) 3822481-3

49-21-73

(8)

Machine Diameter D to remove damage. Metal spray repair Diameter Q, B and/or D. Refer to Figure 601 (Sheet 6). Balance the impeller. Refer to SPM 20-00-02/70-00-01, Method 412B. Shot peen the impeller.

(9)

Weld repair of blade leading edge & contour (REPAIR OUTSIDE)

(10)

Grind repair of curvic (REPAIR OUTSIDE)

(6) (7)

Prepared by: Mohammad Andito / 532006

Replace damaged inlet Part No. 3602679-2

(5)

(4) TRP/49-21/065

Replace Torus Ring Part No. 968509-1 Repair cracked containment ring

(3)

65

Repair cracked torus skin

(2)

(4A)

64

DESCRIPTION

Page 18 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (11)

Weld repair of curvic (REPAIR OUTSIDE)

(12)

Weld repair of Dia Q, B and/or Surface A (REPAIR OUTSIDE)

(13)

Replace curvic coupling and barrel (REPAIR OUTSIDE)

(1)

Straighten repair of bent blade condition.

(2)

Remove nicks, dents, rubs, or other blade damage. Hand finish repair of nicks, dents or vibroscribe markings from backface. Hand finish repair of raised material in curvic tooth surface.

(3) (4) (5) 66

TRP/49-21/066

SECOND STAGE COMPRESSOR ROTOR

(7)

Machine Diameter D to remove damage. Metal spray repair Diameters B, C and/or D. Refer to Figure 601 (Sheet 6). Balance the impeller.

(8)

Shot peen the impeller.

(9)

Weld repair of blade leading edge & contour (REPAIR OUTSIDE)

(10)

Grind repair of curvic (REPAIR OUTSIDE)

(11)

Weld repair of curvic (REPAIR OUTSIDE)

(12)

Weld repair Diameters Q, B and/or Surface A (REPAIR OUTSIDE)

(13)

Replace curvic coupling and barrel (REPAIR OUTSIDE)

(1)

Repair cracked scroll skin

(2)

Repair damaged scroll skin (Inconel 617). Replace damaged inlet flange Remove the old inlet flange and install new Inlet Flange Part No. 3830350-7001 Replace damaged inlet flange. Remove the old inlet flange and install a new Inlet Flange Part No. 3617056-1 Replace damaged studs

(6) 3822536-1/-2

49-21-73

(3) 67

TRP/49-21/067

TURBINE SCROLL HOUSING

3830350-1/-2/-3/4

49-21-73

(3A) (4)

Prepared by: Mohammad Andito / 532006

DESCRIPTION

(1) A

Replace worn or damaged ring and shield assembly.

(1)B

Replace damaged ring and cone assembly

(1)C

Replace damaged flange. Page 19 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

(1)

68

69

TRP/49-21/068

TRP/49-21/069

WHEEL AND SHAFT ASSEMBLY

WHEEL AND SHAFT ASSEMBLY

3842072-1/-2/-3

49-21-73

49-21-73

Repair or Secure loose cupped expansion plug in shaft

(2)(11)

Replace shaft assembly

(3)

Repair turbine wheel blade trailing edge damage

(4)

Repair turbine wheel saddle area damage

(5)

Repair turbine wheel blade tip cracks and erosion

(6)

Repair turbine wheel blade tip impact damage

(7)

(9)

Repair turbine wheel blade leading edge minor damage Repair turbine wheel blade leading edge damage if beyond step (7) limits Repair turbine wheel blade contour, Surface G, damage

(10)

Balance wheel and shaft assembly

(11)

Repair internal diameter of shaft to salvage part.

(12) (13)

Repair outside dimensions of salvaged shaft by metal spray Drill two new pin holes in salvaged shaft 90 degrees from existing holes Remarking Part No. and Serial No.

(1)

Repair shaft assembly

(1)(c)

Repair or Secure loose cupped expansion plug in shaft

(2)(11)

Replace shaft assembly

(3)

Repair turbine wheel blade trailing edge damage

(4)

Repair turbine wheel saddle area damage

(5)

Repair turbine wheel blade tip cracks and erosion

(6)

Repair turbine wheel blade tip impact damage

(7)

Repair turbine wheel blade leading edge minor damage

(8) (9) Prepared by: Mohammad Andito / 532006

Repair shaft assembly

(1)(c)

(8)

3842350-1

DESCRIPTION

Repair turbine wheel blade leading edge damage if beyond step (7) limits Repair turbine wheel blade contour, Surface G, damage Page 20 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (10)

Balance wheel and shaft assembly

(11)

Repair internal diameter of shaft to salvage part.

(12) (13)

(1)

70

TRP/49-21/070

WHEEL AND SHAFT ASSEMBLY

3842360-1

49-21-73

DESCRIPTION

Repair outside dimensions of salvaged shaft by metal spray repair Drill two new pin holes in salvaged shaft 90 degrees from existing holes. Remarking Part No. and Serial No.

Repair shaft assembly

(1)(c)

Repair or Secure loose cupped expansion plug in shaft

(2)(11)

Replace shaft assembly

(3)

Repair turbine wheel blade trailing edge damage

(4)

Repair turbine wheel saddle area damage

(5)

Repair turbine wheel blade tip cracks and erosion

(6)

(9)

Repair turbine wheel blade tip impact damage Restore turbine blade wheel tips (ORI No. T-37827) to repair blade tips damaged from erosion or impact (REPAIR OUTSIDE) Repair turbine wheel blade leading edge minor damage Repair turbine wheel blade leading edge damage if beyond step (7) limits Repair turbine wheel blade contour, Surface G, damage

(10)

Balance wheel and shaft assembly

(6A) (7) (8)

Remarking Part No. and Serial No.

71

TRP/49-21/071

SEGMENTED TURBINE NOZZLE

Prepared by: Mohammad Andito / 532006

3846484-3/-4/-7/8

49-21-73

(1)

Remove cracks or feathering

(2)

Repair erosion and corrosion

(3)

Recoat nozzle

(4)

Reapply aluminum coating to repaired areas

Page 21 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

(2)

Repair cracks (all locations including but not limited to Hub, Flange, Vanes, and weld) by fusion arc (TIG) weld. Repair threads in bolt holes that are damaged beyond chasing

(3)

Repair oversized thread in forward flange

(4)

Replace threaded flange.

(5)

Replace exhaust hub

(1)

72

TRP/49-21/072

EXHAUST DUCT

3850089-1

49-21-73

DESCRIPTION

Modification GTCP85-49-7140

73

TRP/49-21/073

TURBINE PLENUM ASSEMBLY

(1)(3)(4) 692360

49-21-73

(2)(3)(4)

(1)

Repair damaged magnesium surfaces

(2)

(4)

Repair anodized aluminum parts. Repair chipped, scratched or damaged painted or primed surfaces. Prepare parts for repainting exterior surfaces only.

(5)

Replace studs and inserts.

(6)

Repair steel parts.

(7)

Replace loose, worn or damaged bushings.

(8)

Replace bushings (30 through 80 and 180 through 240)

(9)

Repair Diameter FE and/or A to get dimensional limits

(10)

Repair minor damage to Surface BB.

(11)

Repair alignment pin bushing

(3)

74

TRP/49-21/074

MATCHED HOUSING ASSEMBLY SET

693531/-4/-153/100/-100-153/100-4/-150/-150153/-200/-200153/-200-4

49-21-73

(12)

Repair output housing assembly oil passage

(13)

Repair output housing assembly high speed pinion bore

(14)

Repair input housing assembly ribs

(15)

Repair cracked lug for hole number 7. Replace nozzle and stud assembly (Part No. 693531-153/-100-153/-150-153)

(16)

Prepared by: Mohammad Andito / 532006

Repair crack in weld seam (item 1) Repair crack in welded seam and adjoining material (item 2) and crack in intersecting welded seam (item 3) by patching

Page 22 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (17)

Repair the oil jet bore by installation of a threaded sleeve

(18)

Repair idler spur gearshaft boss, Centerline VII

(19)

Repair Gouging and Scoring.

(20)

Repair 2.8745-2.8755 Diameter E by application of metal spray. Plug repair damaged threads (9/16-18UNJF-3B) at AN-6 Oil Port on thin half of Gearbox Housing.

(21) 75

76

77

TRP/49-21/075

TRP/49-21/076

TRP/49-21/077

FORWARD TURBINE SEAL

COMPRESSOR INLET PLENUM ASSEMBLY

COMPRESSOR INLET PLENUM ASSEMBLY

Prepared by: Mohammad Andito / 532006

693616/-1

694016-1/-2/-4

694017

49-21-73

49-21-73

49-21-73

DESCRIPTION

(1)

Repair seal housing

(1)

Repair cracks (items I and 3)

(2)

Repair crack in welded seam and adjoining material (item 2)

(3)

Repair damaged nut plates

(4)

Replace damaged or loose insulator strip (item 5)

(5)

Replace damaged or loose insulating strip (Item 4)

(6)

Replace plenum assembly clamp

(7)

Apply butoxy coating to inside of inlet plenum assembly

(1)

Repair cracks (items I and 3)

(2)

Repair crack in welded seam and adjoining material (item 2)

(3)

Repair damaged nut plates

(4)

Replace damaged or loose insulator strip (item 5)

(5)

Replace damaged or loose insulating strip (Item 4)

(6)

Replace plenum assembly clamp

(7)

Apply butoxy coating to inside of inlet plenum assembly

Page 23 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

78

79

80

81

82

CAPABILITY LIST NO.

TRP/49-21/078

TRP/49-21/079

TRP/49-21/080

TRP/49-21/081

TRP/49-21/082

PART NAME

COMPRESSOR INLET PLENUM ASSEMBLY

OIL TUBE ASSEMBLY

EXHAUST DUCT FLANGE ASSEMBLY

COMBUSTOR CAP ASSEMBLY

COMPRESSOR INLET PLENUM ASSEMBLY

PART NUMBER

694018

694040

695140-1/-50/100/-110

695142-2/-6

695145-100/-101/102

ATA REFERENCE

49-21-73

49-21-73

49-21-73

49-21-73

49-21-73

REPAIR SCHEME

(1)

Repair crack in welded seam and adjoining material (item 3)

(2)

Repair cracks (items I and 2)

(3)

Repair damaged nut plates

(4)

Replace damaged or loose insulator strip (item 5)

(5)

Replace damaged or loose insulating strip (Item 4)

(6)

Apply butoxy coating to inside of inlet plenum assembly

(1)

Repair oil tube assembly

(1)

Repair cracks

(2)

Replace exhaust duct flange

(3)

Ensure exhaust flange feature tolerances

(4)

Replace boss plat

(5)

Replace damaged flange

(1)

Cold straighten combustor cap assembly

(2)

Weld repair cracks in combustor cap assembly

(4)

Repair combustor cap assembly atomizer mounting surface.

(1)

Repair crack (insert A) (item 2) by patching

(2)

Repair cracks (items 1, 3 and 5)

(3)

Remove damaged nut plates (item 4)

(4)

Weld repair cracks or weld brackets to prevent cracking Repair damage to Kynar coating on plenum flange that mates with second stage diffuser housing Replace damaged sound-proofing material with felt cutting material

(5) (6)

Prepared by: Mohammad Andito / 532006

DESCRIPTION

Page 24 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

83

CAPABILITY LIST NO.

PART NAME

TRP/49-21/083

COMBUSTOR CAP ASSEMBLY

PART NUMBER

695709-2/-4

ATA REFERENCE 49-21-73

REPAIR SCHEME

DESCRIPTION

(1)

Cold straighten combustor cap assembly

(2)

Weld repair cracks in combustor cap assembly

(4)

Repair combustor cap assembly atomizer mounting surface.

84

TRP/49-21/084

BEARING CARRIER

695753-1

49-21-73

(1)

Repair Diameter A or B

85

TRP/49-21/085

TUBE FITTINGS MOUNTING BRACKET

696080-1/-2

49-21-73

(1)

Repair weld cracks

49-21-73

(1) (1)(c) (1)(d) (2)(13)(14) (3) (4) (5) (6) (7)

86

TRP/49-21/086

WHEEL AND SHAFT ASSEMBLY

696161-1/-2/-4/7/-8

(11) (12) (13) (14)

Repair shaft assembly Secure loose cupped expansion plug in shaft Repair damage or wear to internal spline area of shaft Replace shaft assembly Repair turbine wheel backface (Surface J) damage Repair turbine wheel saddle area (surface JL) damage Repair turbine wheel blade tip cracks and erosion damage Repair turbine wheel blade contour, Surface G, damage Repair exducer portion of wheel and shaft assembly Repair turbine wheel exducer blade tip damage if not bent more than 30 degrees. More than 30 degrees Repair turbine wheel exducer, cracks at blade trailing edge (Part No. 696161-1/-2/-4) Do a resonant frequency check of exducer blades after repair with an alternate test set Remove and replace exducer Balance wheel and shaft assembly Repair internal diameter of shaft to salvage part Install a replacement wheel on Shaft Part No. 968662-1.

(1)

Cold straighten combustor cap assembly

(2)

Weld repair cracks in combustor cap assembly

(4)

Repair combustor cap assembly atomizer mounting surface.

(8) (9) (10)

87

TRP/49-21/087

COMBUSTOR CAP ASSEMBLY

Prepared by: Mohammad Andito / 532006

696553-1

49-21-73

Page 25 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

88

CAPABILITY LIST NO.

TRP/49-21/088

PART NAME

SUPPORT ASSEMBLY

PART NUMBER

696658-1/-2/-3

ATA REFERENCE

49-21-73

REPAIR SCHEME (1)

Replace damaged ring of support assembly.

(2)

Repair support assembly

(3)

Repair support assembly if cracks are evident in Area J

(4)

Repair damaged or missing bolt holes and scallops

(5)

Repair fretting on surface D

(6)

Repair out of round Dia. A & under sized dia. B by metal spray

(7)

Repair fretting on surface G

(1)(2)(3) (4)

89

TRP/49-21/089

BEARING HOUSING ASSEMBLY

696659-110/-120/140/-160/-170

49-21-73

(5) (6) (7) (8) (10) (11) (12) (14) (15) (16) (17) (18)

Repair cracked damage. Repair damaged Diameter D shows fretting of 0.025 inch or more in depth. Repair damaged surface M and N. Repair damaged Surface P Repair damaged inside diameter of sleeve Replace bearing housing assembly sleeve

(19)

Replace damaged oil tube in housing assembly

(20)

Repair leakage of bearing housing assembly by replacing ring

(21)

(Part No. 696659-70) Replace deswirl vanes

(22)

Repair damaged threads in tapped flange holes Repair Diameters B and/or W and Surfaces P and/or R by the application of metal spray

(23)

Prepared by: Mohammad Andito / 532006

DESCRIPTION

Page 26 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

(1)

(3)

Repair cracks Repair metal thinning due to corrosion or erosion and deformation Replace cap assembly

(4)

Replace damaged deflector

(5)

Replace damaged cooling skirts

(6)

Replace damaged discharge ring

(7)

Replace damaged spacers

(8)

Replace floating grommet

(1)

Weld repair cracks

(2)

Replace damaged nut plates

(1)

Straighten repair of bent blade condition.

(2)

Remove nicks, dents, rubs, or other blade damage.

(3)

Hand finish repair of raised material in curvic tooth surface.

(4)

Machine Diameter B to remove damage.

(5)

Balance the impeller.

(6)

Shot peen the impeller.

(7)

Weld repair of blade leading edge & contour (REPAIR OUTSIDE)

(8)

Grind repair of curvic (REPAIR OUTSIDE)

(9)

Weld repair of curvic (REPAIR OUTSIDE)

(10)

Weld repair Diameter D and/or Surface F (REPAIR OUTSIDE)

(11)

Replace curvic coupling and barrel (REPAIR OUTSIDE)

(2)

90

91

92

TRP/49-21/090

TRP/49-21/091

TRP/49-21/092

COMBUSTION CHAMBER LINER ASSEMBLY

EXHAUST DUCT FLANGE ASSEMBLY

FIRST STAGE IMPELLER

Prepared by: Mohammad Andito / 532006

698168-1 THROUGH -8

698170-1

698192-2/-4

49-21-73

49-21-73

49-21-73

DESCRIPTION

Page 27 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (1)

Straighten repair of blades bent condition.

(2)

Remove nicks, dents, rubs, or other blade damage. Hand finish repair of nicks, dents or vibroscribe markings from backface. Hand finish repair of raised material in curvic tooth surface

(3) (4) (5)

(8)

Machine Diameter D to remove damage. Metal spray repair Diameters B, C and/or D. Refer to Figure 601 (Sheet 6). Balance the impeller. Refer to SPM 20-00-02/70-00-01, Method 412B. Shot peen the impeller.

(9)

Weld repair of blade leading edge & contour (REPAIR OUTSIDE)

(10)

Grind repair of curvic (REPAIR OUTSIDE)

(11)

Weld repair of curvic (REPAIR OUTSIDE)

(12)

Weld repair Diameters B, C and/or Surface A (REPAIR OUTSIDE)

(13)

Replace curvic coupling and barrel (REPAIR OUTSIDE)

(6) 93

TRP/49-21/093

SECOND STAGE IMPELLER

698193-2/-4

49-21-73

(7)

(1)

Repair loose or damaged Inserts.

(2)

Repair damaged Vane.

(6)

Rework diffuser to incorporate steel vanes

(7)(a)

94

TRP/49-21/094

FIRST STAGE DIFFUSER

698194-1

49-21-73

Rework Surfaces A and C.

(7)(b)(1)

Rework Surfaces A

(7)(b)(2)

Rework Surfaces C

(8)(a)

Rework Diameter AC and DC

(8)(b)(1)

Rework Diameter AC by Metal Spray.

(8)(b)(2)

Rework Diameter DC by Metal Spray.

(9)

Repair the vane tips by weld repair to remove erosion

(10)

Weld repair vane tips to clean up erosion Repair the fretting and/or corrosion damage to the port flange surfaces.

(11)

Prepared by: Mohammad Andito / 532006

DESCRIPTION

Page 28 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (1)

Replace damaged or loose inserts and studs

(2)

If examination revealed corrosion in O-ring groove (Detail A)

(2A) (2B)

Repair Diameter P Repair Surface FF

(5)(a)

Repair Surface HH

(5)(b)

Repair Surface HH and UU using metal spray

(6)(a)

Repair Surface AA

(6)(b)

Repair Surface AA using metal spray

(7A)

95

TRP/49-21/095

49-21-73

(13) (14)

(Alternate Method 3) Replace shroud contour

(15)

Repair cracks or stripped threads in mounting pads

(15A) (16) (17) (18)(a) (18)(b) (19) (20) (21) (22) (23) (24) (25)

Prepared by: Mohammad Andito / 532006

Repair Corrosion damage Repair Heavy Corrosion damage at Air flow area. (Recommended Method) Replace shroud contour with a Flanged Sleeve Part No. 966664-1 or –2. (Alternate Method 2) Replace shroud contour

(11A) 698195-1 THROUGH -5/-7/8/-10/-12

Repair O-ring groove if corrosion is more than machining limits

(3)(3A)(4)

(7)

SECOND STAGE DIFFUSER HOUSING ASSEMBLY

DESCRIPTION

Repair cracks next to mount pads Repair stripped or damaged threads in housing assembly Repair Diameter Q with metal spray. Refer to SPM, Method 403D and Table 603 Repair Diameters A and B and face of groove Repair Diameter A, face of groove and Diameter B (Alternate metal spray method). Sleeve corroded or damaged bolt holes on 9.800 inches or 17.25 in. diameter bolt circle Repair Surface FF by installing ring Repair Surface UU with plate Weld repair the outer edge of packing groove Repair Thread Hole Blow out per SB GTCP85-49-7638 (Permanent Repair – Applies only if the APU is to be disassembled) Page 29 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

(26)

Repair Thread Hole Blow out per SB GTCP85-49-7638 (Temporary Repair – Applies only if the APU is not to be disassembled) Repair damaged coating.

(27)

Repair Light damage on Surface UU

(28)

Repair Heavy Corrosion damage at Surface FF. (Alternate Method) Repair by Replace shroud contour with fabricate a Flanged Sleeve

(25)

(12)

(1)(a)

Repair Surface F.

(1)(b)

Repair Surface F by Metal Spray.

(2)

TRP/49-21/096

INLET ASSEMBLY

698197-1/-2

49-21-73

(3)(a)

Rework Surface C to limit of Dimension J Rework Surface C to limit of Dimension J by Metal Spray Repair Surface F by fabricate sleeve.

(5)(a)

Repair/Rework Diameter B

(5)(b)

Repair/Rework Diameter B by Metal Spray

(5)(c)

Repair/Rework Diameter B by fabricate sleeve

(6)

Repair Diameter Q to dimensional limits.

(7)

Rework Diameter CA. See Sheets 10 through 13.

(7A) (8)

Prepared by: Mohammad Andito / 532006

Repair Diameter A to get dimensional limits

(3)(b) (4) 96

DESCRIPTION

Repair Surface D by Wire Arc metal spray. Repair Diameter A, if damaged beyond metal spray limits, by installing a sleeve Repair damaged coating.

Page 30 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

(1)(a)

Repair Surface F

(1)(b)

To repair major rubs

(1A)

Repair Diameter A

(2)

97

TRP/49-21/097

INTERSTAGE HOUSING ASSEMBLY

698198-1

49-21-73

DESCRIPTION

Repair Diameter B

(3)(a)

Surface E can be reworked to establish parallelism

(3)(b)

(4)

Surface E by Metal Spray Repair pitting and other corrosion damage on duct mounting flanges Repair Surface F by replace shroud contour

(5)

Repair damage on Diameter B

(3A)

(6)(a)

Repair Diameter C

(6)(b)

Repair Diameter C by Metal Spray

(6)(c)

Repair Diameter C by Sleeve Repair damaged coating.

98

99

TRP/49-21/098

TURBINE PLENUM ASSEMBLY

TRP/49-21/099

COMBUSTOR CAP ASSEMBLY

(1)(3)(4) 698400-1/-2/-3

698402-1

49-21-73

49-21-73

(2)(3)(4)

Repair crack in weld seam (Item 1) Repair crack in welded seam and adjoining material (Item 2) and crack in intersecting welded seam (Item 3) by patching

(1)

Cold straighten combustor cap assembly

(2)

Weld repair cracks in combustor cap assembly

(4)

Repair combustor cap assembly atomizer mounting surface.

100

TRP/49-21/100

EXHAUST FLANGE ASSEMBLY

698406-1/-2/-3

49-21-73

(1)

Weld repair cracks

101

TRP/49-21/101

PINION GEAR

698816

49-21-73

(1)

Repair Diameter A or B

Prepared by: Mohammad Andito / 532006

Page 31 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

102

CAPABILITY LIST NO.

TRP/49-21/102

PART NAME

GENERATOR DRIVE SPUR GEAR ASSEMBLY

PART NUMBER

698817

ATA REFERENCE

49-21-73

REPAIR SCHEME

DESCRIPTION

(1)

Repair loose plug in gear assembly.

(2)

Repair Diameter A or B

(3)

Balance generator drive spur gear assembly.

(4)

Repair Output drive gearshaft assembly gear teeth

103

TRP/49-21/103

SPUR GEAR

698818-1

49-21-73

(1)

Repair Diameter A or B if inspection reveals damage.

104

TRP/49-21/104

SPUR GEAR

698819

49-21-73

(1)

Repair Diameter A or B if inspection reveals damage.

105

TRP/49-21/105

SPUR GEAR

698820

49-21-73

(1)

Repair Diameter A or B if inspection reveals damage

106

TRP/49-21/106

PLANET GEAR BUSHING

74340

49-21-73

(1)

Repair worn or damaged lead plating on bushing

107

TRP/49-21/107

DRIVE GEAR ASSEMBLY

75331-2/-4

49-21-73

(1)

Repair drive gear pin holes

(2)

Repair bearing diameter of gear

108

TRP/49-21/108

VANE HOUSING ASSEMBLY

75970

49-21-73

(1)

Remove nicks, burrs, or rub marks (Item 1)

(2)

If inserts (Item 2) are loose or damaged

109

TRP/49-21/109

HUB AND FAN ASSEMBLY

75973

49-21-73

(1)

Repair fan assembly

110

TRP/49-21/110

ACCESSORY DRIVE SHAFT ASSEMBLY

76081-6

49-21-73

(1)

Repair drive shaft assembly

(1) TRP/49-21/111

FAN AIR INLET PLENUM ASSEMBLY

Repair cracks (items 1 and 3) Repair crack in welded seam and adjoining material (item 2) by patching Remove damaged nut plates (item 4)

111

76098

49-21-73

(2) (3)

Prepared by: Mohammad Andito / 532006

Page 32 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

112

113

114

CAPABILITY LIST NO.

TRP/49-21/112

TRP/49-21/113

TRP/49-21/114

PART NAME

SECOND STAGE COMPRESSOR DIFFUSER

AIR DUCT ASSEMBLY

COMPRESSOR INLET PLENUM ASSEMBLY

PART NUMBER

892290-1/-2/-4

892292-1/-2/-3/4/-5/-6/-7

892294-1/-2/-3/-4

ATA REFERENCE

49-21-73

49-21-73

49-21-73

REPAIR SCHEME (1)

Repair damaged Surface E

(2)

Repair damaged vane leading edge

(4)

Repair damaged Diameter D

(5)

Repair damaged Diameter C

(3)

If visual check revealed damaged paint areas on vanes

(1)

Repair duct assembly fiberglass, nutplate and gasket

(2)(3)(4)

Replace small and large flange

(2)(4)

Repair damaged flange by weld

(1)

Repair cracks (Items 1 and 3)

(2)

Repair crack in welded seam and adjoining material (item 2)

(3)

Remove damaged nut plates

(1)

(3)

Repair cracks Repair metal thinning due to corrosion or erosion and deformation Replace cap assembly

(4)

Replace damaged deflector

(5)

Replace damaged cooling skirts

(6)

Replace damaged discharge ring

(7)

Replace damaged spacers

(8)

Replace floating grommet

(2)

115

TRP/49-21/115

COMBUSTION CHAMBER LINER ASSEMBLY

899155-1/-2/-3/4/-5

49-21-73

(9)(a) (9)(b) (10)

Prepared by: Mohammad Andito / 532006

DESCRIPTION

(Part No. 899155-4/-5) Replace damaged wiggle strip Replace damaged wiggle strip by replacing entire discharge ring. Apply thermal barrier coating to the inside surface of the combustor

Page 33 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (1)

(3)

Repair cracks Repair metal thinning due to corrosion or erosion and deformation Replace cap assembly

(4)

Replace damaged deflector

(5)

Replace damaged cooling skirts

(6)

Replace damaged discharge ring

(7)

Replace damaged spacers

(8)

Replace floating grommet

(2)

116

TRP/49-21/116

COMBUSTION CHAMBER LINER ASSEMBLY

899244-1/-2/-3/4/-5

49-21-73

(2)

Cold straighten combustor cap assembly dents to necessary dimensions Weld repair cracks in combustor cap assembly

(4)

Repair combustor cap assembly atomizer mounting surface

(1)

Repair cracks with weld.

(1)

Repair cracked in torus skin

(1) 117

118

119

TRP/49-21/117

TRP/49-21/118

TRP/49-21/119

COMBUSTOR CAP ASSEMBLY

OIL COOLER BRACKET

TURBINE TORUS ASSEMBLY

899323-1/-2/-3/-4

899331-1/-2

899373-1/-2/-3/-3359

49-21-73

49-21-73

(1A)

Repair cracks in weld

(1B)

Replace the Torus Ring Part No. 968509-1

(2)

(5)

Repair cracked containment ring Repair damaged torus skin (Inconel 600 or Hastelloy X stock) by patching Replace damaged inlet flange (Haynes 25 stock). Remove the old inlet flange and install new Inlet Flange Part No. 3602679-1 Replace damaged inlet flange (Haynes 25 stock). Remove the old inlet flange and install a new Inlet Flange P/N 3602679-2 Replace damaged studs

(6)

Replace damaged ring and shield assembly

(7)

Replace damaged cover assembly

(3) 49-21-73

(4) (4A)

Prepared by: Mohammad Andito / 532006

DESCRIPTION

Page 34 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

120

TRP/49-21/120

TURBINE PLENUM ASSEMBLY

899374-1

49-21-73

121

TRP/49-21/121

EXHAUST PIPE ASSEMBLY

899607-1

49-21-73

REPAIR SCHEME

(1)(3)(4) (2)(3)(4)

(1)

(1)

122

123

124

TRP/49-21/122

TRP/49-21/123

TRP/49-21/124

TURBINE SEAL

FIRST STAGE IMPELLER

Prepared by: Mohammad Andito / 532006

899930-1/-3

899987-1

966568-1

49-21-73

49-21-73

49-21-73

Repair crack in weld seam (item 1) Repair crack in welded seam and adjoining material (Item 2) and crack in intersecting welded seam (item 3) by patching Repair Procedures - DELETED. Part has to be reworked per Service Bulletin 49-A5078

(3)

Repair cracks Repair metal thinning due to corrosion or erosion and deformation Replace cap assembly

(4)

Replace damaged deflector

(5)

Replace damaged cooling skirts

(6)

Replace damaged discharge ring

(7)

Replace damaged spacers

(8)

Replace floating grommet

(1)

Repair housing

(1)

Straighten repair of bent blade condition.

(2)

Remove nicks, dents, rubs, or other blade damage.

(3)

Hand finish repair of raised material in curvic tooth surface.

(4)

Machine Diameter B to remove damage.

(5)

Balance the impeller.

(6)

Shot peen the impeller.

(7)

Weld repair of blade leading edge & contour (REPAIR OUTSIDE)

(8)

Grind repair of curvic (REPAIR OUTSIDE)

(9)

Weld repair of curvic (REPAIR OUTSIDE)

(2) COMBUSTION CHAMBER LINER ASSEMBLY

DESCRIPTION

Page 35 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

DESCRIPTION

(10)

Weld repair Diameter D and/or Surface F (REPAIR OUTSIDE)

(11)

Replace curvic coupling and barrel (REPAIR OUTSIDE) Remarking Part No. and Serial No.

125

126

TRP/49-21/125

TRP/49-21/126

SECOND STAGE COMPRESSOR ROTOR

FIRST STAGE IMPELLER

966569-1/-2

966570-1

49-21-73

49-21-73

(1)

Straighten repair of bent blade condition.

(2)

Remove nicks, dents, rubs, or other blade damage.

(3)

Hand finish repair of raised material in curvic tooth surface.

(4)

Machine Diameter B to remove damage.

(5)

Balance the impeller.

(6)

Shot peen the impeller.

(7)

Weld repair of blade leading edge and contour.

(8)

Grind repair of curvic.

(9)

Weld repair of curvic (REPAIR OUTSIDE)

(10)

Weld repair Diameter D and/or Surface F (REPAIR OUTSIDE)

(11)

Replace curvic coupling and barrel (REPAIR OUTSIDE)

(1)

Straighten repair of bent blade condition.

(2)

Remove nicks, dents, rubs, or other blade damage.

(3)

Hand finish repair of raised material in curvic tooth surface.

(4)

Machine Diameter B to remove damage.

(5)

Balance the impeller.

(6)

Shot peen the impeller.

(7)

Weld repair of blade leading edge & contour (REPAIR OUTSIDE)

(8)

Grind repair of curvic (REPAIR OUTSIDE)

(9)

Weld repair of curvic (REPAIR OUTSIDE)

(10)

Weld repair Diameter D and/or Surface F (REPAIR OUTSIDE)

(11)

Replace curvic coupling and barrel (REPAIR OUTSIDE) Remarking Part No. and Serial No.

Prepared by: Mohammad Andito / 532006

Page 36 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (1)

Straighten repair of blades bent condition.

(2)

Remove nicks, dents, rubs, or other blade damage. Hand finish repair of nicks, dents or vibroscribe markings from backface. Hand finish repair of raised material in curvic tooth surface

(3) (4) (5)

(7)

Machine Diameter D to remove damage. Metal spray repair Diameters B, C and/or D. Refer to Figure 601 (Sheet 6). Balance the impeller. Refer to SPM, Method 412B.

(8)

Shot peen the impeller.

(9)

Weld repair of blade leading edge & contour (REPAIR OUTSIDE)

(10)

Grind repair of curvic (REPAIR OUTSIDE)

(11)

Weld repair of curvic (REPAIR OUTSIDE)

(12)

Weld repair Diameters B, C and/or Surface A (REPAIR OUTSIDE)

(13)

Replace curvic coupling and barrel (REPAIR OUTSIDE)

(6) 127

128

TRP/49-21/127

TRP/49-21/128

SECOND STAGE IMPELLER

BEARING HOUSING ASSEMBLY

966571-1

966578-9/-11/12/-13

49-21-73

49-21-73

(1) (2) (3)

Repair cracked damage.

(4) (5) (6) (7) (8) (10) (11) (12) (13) (14) (15) (16) (17)

Repair damaged Diameter D Repair damaged Surfaces M and N (Preferred Method) Repair damaged Surfaces P and R Repair damaged inside diameter of sleeve (Diameter F) Replace deswirl vanes

(18)

Replace bearing housing assembly sleeve

(19)

Replace damaged oil tube in housing assembly

(20)

Repair leakage of bearing housing assembly by replacing ring

(21)

Repair damaged threads in tapped flange holes Repair Diameters B and/or W and Surfaces P and/or R by the application of metal spray

(22) Prepared by: Mohammad Andito / 532006

DESCRIPTION

Page 37 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

129

CAPABILITY LIST NO.

TRP/49-21/129

PART NAME

EXHAUST PIPE ASSEMBLY

PART NUMBER

966580

ATA REFERENCE

49-21-73

REPAIR SCHEME

(1)

Repair weld cracks in tube wall

(2)

Repair weld circumferential cracks in radius of flange

(3)

(5)

Repair cracked weld or brazed joint in Area A Repair threads in bolt holes that are damaged beyond simple repair Repair oversize thread in forward flange

(6)

Replace threaded flange

(1)(a)

Repair cracked torus skin

(1)(b)

Repair cracks in seam weld using Hastelloy X stock

(2)(a)

(5)

Repair cracked forged ring Erosion on inside surface of forged ring exceeding 0.100 inch or leaving less than 0.075 inch thickness Cracks in stud bolt areas shall be repair welded Repair damaged torus skin (Inconel 600 or Hastelloy X stock) by patching Replace damaged inlet flange (Haynes 25 stock). Remove the old inlet flange and install new Inlet Flange Part No. 3602679-1 Replace damaged inlet flange (Haynes 25 stock). Remove the old inlet flange and install a new Inlet Flange Part No. 3602679-2 Replace damaged studs

(6)

Replace damaged ring and shield assembly

(7)

Replace damaged cover assembly

(4)

(2)(b) (2)(c) 130

TRP/49-21/130

TURBINE TORUS ASSEMBLY

966582-1/-2/-6/8 through -12/14 through -28

49-21-73

(3) (4) (4A)

131

TRP/49-21/131

TURBINE WHEEL SHROUD

Prepared by: Mohammad Andito / 532006

966583-1

49-21-73

DESCRIPTION

(1)(a)(b)

Repair turbine wheel shroud

(1)(c)

Repair damaged Diameter A

(1)(d)

Repair damaged Diameter B

(1)(e)

Repair damaged bolt holes.

Page 38 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

132

CAPABILITY LIST NO.

TRP/49-21/132

PART NAME

SUPPORT ASSEMBLY

PART NUMBER

966584-1 THROUGH -5

ATA REFERENCE

49-21-73

REPAIR SCHEME (1)

Replace damaged ring of support assembly.

(2)

Repair support assembly.

(3)

Repair support assembly if cracks are evident in Area J

(4)

Repair damaged or missing bolt holes and scallops

(5)

(7)

Repair fretting on surface D Repair out of round Dia. A and under sized diameter B by metal spray Repair fretting on surface G

(1)

Repair shaft assembly

(6)

(1)(c)

Secure loose cupped expansion plug in shaft

(1)(d)

Repair damage or wear to internal spline area of shaft

(2)(13)(14)

133

TRP/49-21/133

WHEEL AND SHAFT ASSEMBLY

966625-1/-2/-4/7/-8

49-21-73

Replace shaft assembly

(3)

Repair turbine wheel backface (Surface J) damage

(4)

Repair turbine wheel saddle area (surface JL) damage

(5)

Repair turbine wheel blade tip cracks and erosion damage

(6)

Repair turbine wheel blade contour, Surface G, damage

(7)

(11)

Repair exducer portion of wheel and shaft assembly Repair turbine wheel exducer blade tip damage if not bent more than 30 degrees. More than 30 degrees Repair turbine wheel exducer, cracks at blade trailing edge (Part No. 966625-1/-2/-4) Do a resonant frequency check of exclucer blades after repair with an alternate test set Remove and replace exducer

(12)

Balance wheel and shaft assembly

(13)

Repair internal diameter of shaft to salvage part

(8) (9) (10)

(14) (15) (16)

Prepared by: Mohammad Andito / 532006

DESCRIPTION

Install a replacement wheel on Shaft Part No. 968662-1. Repair the fretting and/or corrosion damage to the port flange surfaces

Page 39 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

(1)

TRP/49-21/134

WHEEL AND SHAFT ASSEMBLY

968095-1/-3/-5/-X360

49-21-73

(1)(c)

Secure loose cupped expansion plug in shaft Repair damage or wear to internal spline area of shaft Repair turbine wheel blade trailing edge damage

(4)

Repair turbine wheel saddle area damage

(5)

Repair turbine wheel blade tip cracks and erosion damage

(6)

Repair turbine wheel blade tip impact damage

(7)

Repair turbine wheel blade leading edge minor damage Repair turbine wheel blade leading edge damage if beyond step (7) limits Repair turbine wheel blade contour damaged, Surface G, Balance wheel and shaft assembly. Refer to SPM, Method 412A, 412C Repair internal diameter of shaft to salvage part.

(9) (10) (11)

TRP/49-21/135

COMPRESSOR INLET PLENUM ASSEMBLY

Prepared by: Mohammad Andito / 532006

968098-2

49-21-73

Replace shaft assembly

(3)

(8)

135

Repair shaft assembly

(1)(d) (2)(11)(14)

134

DESCRIPTION

(1)

Repair cracks (items 1 and 3)

(2)

Repair crack in welded seam and adjoining material (item 2)

(3)

Remove damaged nut plates (item 4).

(4)

Replace damaged or loose insulator strip (item 5)

Page 40 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

968233-1/-1-189

ATA REFERENCE

49-21-73

REPAIR SCHEME (1)

If Diameter E is out of tolerance

(2)

Machine a minimum amount of material from Surface M

(3)

Machine Diameters B and C

(4)

If Surface K is not flat to specified limits

(4A)

Repair wear or damage on Diameter B using plasma spray

(6)(7)

Repair cracks in Surface H, by hand finish

(8)

Repair cracks in Surface H, by Machining

(9)

(1)

Repair Threads damage If nozzle spacer contact areas on Surface F are not perpendicular to the limits specified or if spacer fretting of Surface M goes beyond 0.015 inch Repair Diameter E

(2)

Machine a minimum amount of material from Surface M

(3)

Machine Diameters B and C

(4)

If Surface T is not flat to specified limits

(5)

Repair damage contact areas on Surface M less than 0.015 in.

(5) (10) 136

TRP/49-21/136

TURBINE WHEEL SHROUD

968233-4/-4-189

137

TRP/49-21/137

TURBINE PLENUM ASSEMBLY

Prepared by: Mohammad Andito / 532006

49-21-73

(6) (7) (8)

Repair cracks in Surface H, by hand finish

(9)

Repair cracks in Surface H, by Machining

(10)

Repair Threads damage

(11)

Repair damage contact areas on Surface M more than 0.015 in

(1) (3) 968613-1

49-21-73

DESCRIPTION

(2) (3)

Repair crack in weld seam (item 1) Repair crack in welded seam and adjoining material (Item 2) and crack in intersecting welded seam (Item 3)

Page 41 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

138

139

140

141

CAPABILITY LIST NO.

TRP/49-21/138

TRP/49-21/139

TRP/49-21/140

TRP/49-21/141

PART NAME

COMPRESSOR INLET PLENUM ASSEMBLY

EXHAUST DUCT FLANGE ASSEMBLY

EXHAUST DUCT FLANGE ASSEMBLY

CONTAINMENT RING

PART NUMBER

968844-1

968867-1

968886-1/-5

968958-1/-2/-3/-4

ATA REFERENCE

49-21-73

49-21-73

49-21-73

49-21-73

REPAIR SCHEME (1)

Repair cracks (items 1 and 3)

(2)

Repair crack in welded seam and adjoining material (item 2)

(3)

Remove damaged nut plates (item 4).

(4)

Replace damaged or loose insulator strip (item 5)

(5)

Weld loose brackets (Item 5)

(1)

Weld repair cracks

(1)

Remove cracks or feathering on trailing edge

(2)

Repair erosion and corrosion of vane leading edge

(3) (4) (6)

Repair/Machine Diameters A and B Dimensions D

(1)

Repair damaged Ring

(1)

Repair cracked torus skin Repair damaged torus skin (Inconel 600 or Hastelloy X stock) with welded scab patch Replace damaged inlet flange Remove the old inlet flange and install new Inlet Flange Part No. 3602679-1 Replace damaged inlet flange (Haynes 25 stock). Remove the old inlet flange and install a new Inlet Flange Part No. 3602679-2 Replace damaged studs

(2) (2A) (3)

142

TRP/49-21/142

TURBINE TORUS ASSEMBLY

968959-2/-3/-4/5/-8/-9/-11/-12/13/-22/-23/-26

(3A) 49-21-73 (4) (1)1

(1)3

(P/N 968959-2/-3) Replace damaged ring and shield assembly (P/N 968959-4/-5/-8/-9/-11/-12/-13) Replace worn or damaged ring and shield assembly Replace damaged ring and cone assembly

(1)4

(P/N 968959-22/-23/-26) Replace damaged flange

(1)2

Prepared by: Mohammad Andito / 532006

DESCRIPTION

Page 42 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

143

TRP/49-21/143

TURBINE NOZZLE BOLT SPACERS

968969-1/-2

49-21-73

(1)

Repair damaged Surfaces B and C

(1)

Repair minor scratches or rub marks

(2)

Repair fretting or out of flatness of Surface G

(3)

Repair damaged Diameter C

(4)

Repair damaged Diameter B

(5)

Repair nick, dent and scoring

(6)

Repair fretting on Surface Q

(7)

Repair damaged Diameter R

144

TRP/49-21/144

COMBUSTION CHAMBER LINER ASSEMBLY

968984-1/-1-189/4/-4-189

49-21-73

(7)(h)

145

TRP/49-21/145

Prepared by: Mohammad Andito / 532006

969233-1/-2

49-21-73

Repair Cracks in the outer bolts holes

(8)

Repair worn or damaged Diameter B with Metal Spray

(9)

Repair worn or damaged Diameter A.

(10)

Repair worn or damaged Diameter C using metal spray coating

(1)

Repair damaged Surface G

(1)

(3)

Repair cracks Repair metal thinning due to corrosion or erosion and deformation Replace cap assembly

(4)

Replace damaged grommet

(5)

Replace damaged cooling skirts

(6)

Replace damaged discharge ring

(7)

Replace damaged spacers

(2) COMBUSTION CHAMBER LINER ASSEMBLY

DESCRIPTION

Page 43 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

969293-1/-1-189

ATA REFERENCE

49-21-73

REPAIR SCHEME (1)

Repair damaged Diameter E

(2)

Repair damaged Surface M

(3)

Repair damaged Diameter B and C

(4)

Repair damaged Surface B by Metal Spray.

(5)

Repair Surface K

(7) (8)

Repair Cracked damage in Surface H.

(9) (10)

Repair rub marks on Surface H

(11) 146

TRP/49-21/146

TURBINE WHEEL SHROUD

(12) (6)

969293-2/-2-189

49-21-73

148

TRP/49-21/147

TRP/49-21/148

COMPRESSOR INLET PLENUM ASSEMBLY

OIL TANK ASSEMBLY

Prepared by: Mohammad Andito / 532006

976015-1/-5

976036-1/-2/-3/-4

49-21-73

49-21-73

Repair/Chase damaged threads. Repair damaged Surface M Refer to Figure 602 step (1)

(1)

Repair damaged Diameter E

(2)

Repair damaged Surface M

(3)

Repair damaged Diameter B and C

(4)

Repair Surface T

(6) (7)

Repair Cracked damage in Surface H.

(8) (9)

Repair rub marks on Surface H

(10)

Repair/Chase damaged threads

(11)(5)

147

DESCRIPTION

Repair damaged Surface M Refer to Figure 602 step (1)

(1)

Repair cracks (items 1 and 3)

(2)

Repair crack in welded seam and adjoining material (item 2)

(3)

Remove damaged nut plates (item 4).

(4)

Replace damaged or loose insulator strip (item 5)

(5)

Repair damaged thermal lag coating locally or entire area.

(6)

Repair Cracks emanating from slots (item 5).

(1) (2) (3) (4) (5) (6)

Repair Damaged Oil Tank.

Page 44 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

(1)

(4)

Repair crack in weld seam (Item 1) Repair cracks in mounting flange that are not longer than 4 inch length. Repair crack in welded seam and adjoining material (Item 2) and crack in intersecting welded seams (Item 3) by patching. Repair the damaged boss.

(5)

Repair stripped, worn or cut threads.

(6)

Repair stripped worn or stripped holes in nameplate bracket.

(7)

Repair Surface A Flatness.

(8)

Repair Plenum Flange.

(1)

Repair weld cracks (Part No. 976079-4 only) Replace damaged loose or missing patch on face of the exhaust baffle

(2) (3) 149

150

151

TRP/49-21/149

TRP/49-21/150

TRP/49-21/151

TURBINE PLENUM ASSEMBLY

BAFFLE ASSEMBLY

EXHAUST FLANGE ASSEMBLY

Prepared by: Mohammad Andito / 532006

976052-1/-2/-3/4/-5

976079-1/-3/-4

976160-2/-3

49-21-73

49-21-73

49-21-73

DESCRIPTION

(2)

(1)

Weld repair cracks

(2)

Replace fittings

(3)

Replace scupper

(4)

Replace boss

Page 45 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

152

CAPABILITY LIST NO.

TRP/49-21/152

PART NAME

BEARING HOUSING ASSEMBLY

PART NUMBER

976979-1

ATA REFERENCE

49-21-73

REPAIR SCHEME (1)

Repair cracked damage.

(2)

Repair damaged Diameter D

(3)

Repair damaged Surfaces M and N

(4)

(Preferred Method) Repair damaged Surfaces P and R

(5)

Repair damaged inside diameter of sleeve (Diameter F)

(6)

Replace damaged or loose pin

(7)

(Part No. 976979-1/-3) Replace vanes

(8)

Replace bearing housing assembly sleeve

(9)

Replace damaged oil tube in housing assembly

(10)

Repair leakage of bearing housing assembly by replacing ring

(11)

(13)

Repair damaged threads in tapped flange holes Repair Diameters B and/or W and Surfaces P and/or R by the applying metal spray Repair cracked damage on vane

(14)

ULTRASONIC Cleaning as Reference EI No. AG/49-21-0303.

(15)

Repair the Ring Groove by blending and welding

(1)

Repair weld cracks in tube wall

(2)

Repair weld circumferential cracks in radius of flange

(3)

Repair cracked weld or brazed joint in Area A Repair threads in bolt holes that are damaged beyond chasing, tapping and/or suitable insert Repair oversize thread in forward flange

(12)

153

TRP/49-21/153

EXHAUST PIPE ASSEMBLY

976987-1

49-21-73

(4) (5)

154

TRP/49-21/154

FAN AIR INLET PLENUM

Prepared by: Mohammad Andito / 532006

977077-1

49-21-73

DESCRIPTION

(6)

Replace threaded flange Repair threads in bolt holes that are damaged by helicoil insert installation

(1)

Repair fan air line plenum cracks (items 1, 2, and 3)

(2)

Remove and replace damaged nut plates Page 46 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME (1)

155

TRP/49-21/155

TURBINE PLENUM ASSEMBLY

977106-2

49-21-73

(2) (3)

156

TRP/49-21/156

977831-1/-5

49-21-73

Repair damaged magnesium surfaces

(2)

(4)

Repair anodized aluminum parts Repair chipped, scratched or damaged painted or primed surfaces Prepare parts for repainting exterior surfaces only.

(5)

Replace studs and inserts

(6)

Repair steel parts.

(7)

Replace loose, worn or damaged bushings

(8)

Replace bushings (30 through 80 and 180 through 230)

(9)

Repair Diameter FE and/or A to get dimensional limits

(10)

(12)

Repair minor damage to Surface BB Repair alignment pin bushing(s) (90, 260, Sheet 1) if examination reveals damage Repair output housing assembly oil passage

(13)

Repair output housing assembly high speed pinion bore

(14)

Repair input housing assembly ribs

(15)

Repair cracked lug for hole number 7

(16)

(Part No. 977831-5) Replace nozzle and stud assembly

(17)

Repair the oil jet bore by installation of a threaded sleeve

(18)

Repair idler spur gearshaft boss, Centerline V11

(19)

Repair Gouging and scoring to accessory mount bores.

(20)

Repair 2.8745 to 2,8755 inch Dia. E by apply Metal Spray. Plug repair damaged threads (9/16-18UNJF-3B) at AN-6 Oil Port on thin half of gearbox housing.

(11)

(21)

Prepared by: Mohammad Andito / 532006

Repair crack in weld seam (Item 1) Repair crack in welded seam and adjoining material (Item 2) and crack in intersecting welded seams (Item 3) by patching. Heat treatment /stress relieve at approximately 1350 oF (732 oC) f or 30 minutes

(1)

(3)

MATCHED HOUSING ASSEMBLY SET

DESCRIPTION

Page 47 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

157

CAPABILITY LIST NO.

TRP/49-21/157

PART NAME

BEARING HOUSING ASSEMBLY

PART NUMBER

977894-1/-2/-3/8/-9

ATA REFERENCE

49-21-73

REPAIR SCHEME

DESCRIPTION

(1) (2) (3)

Repair cracked damage.

(4) (5) (6) (7) (8) (10) (11) (12) (14) (15) (16) (17) (18)

Repair damaged Diameter D Repair damaged Surfaces M and N (Preferred Method) Repair damaged Surfaces P and R Repair damaged inside diameter of sleeve (Diameter F) Replace vanes (P/N 977894-8)

(19)

Replace vanes (P/N 977894-9)

(20)

Replace bearing housing assembly sleeve

(21)

Replace damaged oil tube in housing assembly

(22)

Repair leakage of bearing housing assembly by replacing ring

(23)

(25)

Repair damaged threads in tapped flange holes Repair Diameters B and/or W and Surfaces P and/or R by metal spray ULTRASONIC Cleaning as Reference EI#AG/49-21-0303.

(24)

158

TRP/49-21/158

TURBINE SEAL

977898-1

49-21-73

(1)

Repair Housing

159

TRP/49-21/159

COVER

3602188-1

49-25-41

(1)

Inspect and repaint part

160

TRP/49-21/160

SEAL RING

3604738

49-21-73

(1)

Inspect Only

(1)

Repair/replace the damaged Rivets and Anchor Nut

(2)

Repair Cracked damage.

(3)

Repair fretted at bolt hole.

(4)

Repaint the green enamel on baffle assembly

161

TRP/49-21/161

BAFFLE ASSEMBLY

Prepared by: Mohammad Andito / 532006

3613511

49-21-73

Page 48 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

162

TRP/49-21/162

CONTAINMENT RING

3616426

49-21-73

(1)

Inspect Only

163

TRP/49-21/163

STARTER PAWL DRIVE JAW

373781-2

49-21-73

(1)

Inspect Only

164

TRP/49-21/164

BEARING RETAINER

379560

49-21-73

(1)

Inspect, remove nick and score, repaint

165

TRP/49-21/165

BEARING RETAINER

379587

49-21-73

(1)

Inspect, remove nick and score, repaint

166

TRP/49-21/166

EXTERNAL HEAT SHIELD

3844783-1/-2

49-21-73

(1)

Inspect Only

167

TRP/49-21/167

EXTERNAL HEAT SHIELD

3844911

49-21-73

(1)

Inspect Only

168

TRP/49-21/168

MAIN DRIVE BEVEL GEAR

73742

49-21-73

(1)

Inspect Only

169

TRP/49-21/169

BEVELED GEAR

73744-2

49-21-73

(1)

Inspect Only

170

TRP/49-21/170

MAIN SHAFT

73749-2/-3/-6

49-21-73

(1)

Inspect Only

171

TRP/49-21/171

GOVERNOR DRIVE GEAR

73848-2

49-21-73

(1)

Inspect Only

172

TRP/49-21/172

CONTAINMENT RING

966581-1

49-21-73

(1)

Inspect Only

173

TRP/49-21/173

TURBINE NOZZLE BOLT

968972-1

49-21-73

(1)

Inspect and remove nick and score

Prepared by: Mohammad Andito / 532006

DESCRIPTION

Page 49 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

CAPABILITY LIST NO.

PART NAME

PART NUMBER

ATA REFERENCE

REPAIR SCHEME

174

TRP/49-21/174

HOUSING FLANGE

969008

49-21-73

(1)

Inspect Only

175

TRP/49-21/175

NOZZLE AND STUD ASSY

969022

49-21-73

(1)

Inspect Only

176

TRP/49-21/176

TORSION SHAFT

969291

49-21-73

(1)

Inspect Only

177

TRP/49-21/177

BEARING RETAINER

969416-1/-2

49-21-73

(1)

Inspect, remove nick and score, repaint

178

TRP/49-90/178

OIL TANK ASSEMBLY

695147

49-90-35

(1)

Inspect Only

179

TRP/49-13/179

BRACKET

65-50964-1

49-13-00

(1)

Inspect, remove nick and score, repaint

180

TRP/49-10/180

STAND ASSEMBLY

65-62580

49-10-21

(1)

Inspect Only

181

TRP/49-21/181

BRACKET

69-50854

49-13-00

(1)

Inspect, remove nick and score, repaint

182

TRP/49-21/182

HOSE

113896

49-25-41

(1)

Inspect, repair damaged rubber

183

TRP/49-90/183

EGT THERMOCOUPLE

304461-2

49-25-45

(1)

Inspect Only

184

TRP/49-21/184

SUPPORT ASSY IGN UNIT

976129

49-25-41

(1)

Inspect Only

(1)

Repair/replace the damaged Rivets and Anchor Nut

(2)

Repair Cracked damage.

(3)

Repair fretted at bolt hole.

(4)

Repaint the green enamel on baffle assembly

185

TRP/49-21/185

BAFFLE ASSEMBLY

Prepared by: Mohammad Andito / 532006

3613615

49-21-73

DESCRIPTION

Page 50 of 51

Revision: 03 / 08 February 2011

Inhouse Capability List Engine GTCP85-Series GMF AeroAsia

NO

186

187

CAPABILITY LIST NO.

TRP/49-21/186

TRP/49-21/187

PART NAME

BAFFLE ASSEMBLY

BAFFLE ASSEMBLY

PART NUMBER

968538-1/-3/-6/7/-8/-9

968539-1/-2

ATA REFERENCE

49-21-73

49-21-73

REPAIR SCHEME

DESCRIPTION

(1)

Repair/replace the damaged Rivets and Anchor Nut

(2)

Repair Cracked damage.

(3)

Repair fretted at bolt hole.

(4)

Repaint the green enamel on baffle assembly

(1)

Repair/replace the damaged Rivets and Anchor Nut

(2)

Repair Cracked damage.

(3)

Repair fretted at bolt hole.

(4)

Repaint the green enamel on baffle assembly

188

TRP/49-25/188

CDP ORIFICE

3605837-2

49-25-45

(1)

Inspect, remove nick and score, repaint

189

TRP/49-25/189

BRACKET

3870127

49-25-41

(1)

Inspect, remove nick and score, re-protect alodine, repaint

190

TRP/49-41/190

IGNITER PLUG LEAD

369259

49-41-05

(1)

Inspect Only

191

TRP/49-41/191

IGNITER PLUG LEAD

3888076

49-41-05

(1)

Inspect Only

192

TRP/49-25/192

HOSE

S9438A04

49-25-41

(1)

Inspect, repair damaged rubber

193

TRP/49-25/193

HOSE

S9438A08

49-25-41

(1)

Inspect, repair damaged rubber

194

TRP/49-50/194

SCREEN ASSY

698423-1

49-50-37

(1)

Inspect, repair damaged hole, repaint

Prepared by: Mohammad Andito / 532006

Page 51 of 51

Inhouse Capability List APU GTCP85 GMF AeroAsia.pdf ...

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