Attachment_0079_-_Critical_Characteristics.pdf

04/27/2017

3024T32P09 6615 01 176 - 3531

N NN

92555

98391

99207

Lee Co

Arkwin Industries Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Jet, ServocylinderNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

CSI Date

Approved Date

M&O CRITICAL SAFETY ITEMS

3033T33G02 2915 01 120 - 8717

N

Y

Y

N

N

N

Y

N

N

Acceptance Test per Army DMWR 55-2915-341

Acceptance Test per drawing (G.E. design specification AMC-CE-2222-02010)

Spline data per note 4 and table (zone G-8 & H-8) of drawing 5034T91; as measured or as verified by spline gauge

51663

99207

Crane Company (Lear Romec Div)

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Pump, Fuel BoostNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

10/01/1987CSI Date

3033T81P04 5330 01 187 - 7837

Y YY Non procurable. If a procurement is required, request CC from AED.

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Ring, SealNoun YCritical Safety

NSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

03/17/1996CSI Date

3046T17G01 2915 01 150 - 2933

Y

N

N

N

N

Y

Acceptance Test per M50TF2467CL-B (see table B9 of drawing 6044T78)

Acceptance test procedure per Army DMWR 55-2995-237

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Valve, OverspeedNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

10/07/1993CSI Date

3046T17G02 2915 01 462 - 3670

Y

N

N

N

N

Y

Acceptance Test per M50TF2467CL-B (see table B9 of drawing 6044T78)

Acceptance test procedure per Army DMWR 55-2995-237

98391

99207

Arkwin Industries Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Valve, OverspeedNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

12/06/1999CSI Date

3048T90G01 2840 01 515 - 3538

Y

Y

N

N

Y

Y

Assembly contains CSI subcomponents

Visual Inspection Verification that all cooling air passages are clear after machining

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Matched Assy, H Pres TurbineNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

11/03/2005CSI Date

3056T17P09 2840 01 509 - 0348

Y

Y

N

N

N

N

N

N

Y

Dovetail Contour per drawing Note 2

FPI per drawing note 6

No Cracks beyond DMWR Limits via White Light Inspection

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 1 Turbine Rotor BladeNoun YCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

11/03/2005CSI Date

3056T17P11 2840 01 509 - 0348

Y

Y

N

N

N

N

N

N

Y

Dovetail Contours per Drawing 3056T17P11, Note 3

FPI per Drawing 3056T17P11, Note 6

No Cracks beyond DMWR Limits via White Light Inspection

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 1 Turbine Rotor BladeNoun YCritical Safety

NSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

07/01/2014CSI Date

3056T94P02 2840 01 509 - 0325

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 1 ShroudNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

3065T21G01 2840 01 482 - 1870

Y NY Assembly contains CSI components

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shaft Assy, TurbineNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

06/08/2010CSI Date

3065T21G04 2840 01 630 - 1878

Y NY Assembly contains CSIs

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shaft Assy, TurbineNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

09/03/2014CSI Date

3065T21G05 2840 01 629 - 7392

Y NY Assembly contains CSIs

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shaft Assy, TurbineNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

09/03/2014CSI Date

3174020-1 5930 01 318 - 3878

N NN

59364

99207

Honeywell Intl Inc Engines and Systems Engine Systems and Accessories ESA

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Cover, Electrical SwitchNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

CSI Date

4040T20P01 3110 01 087 - 4284

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter between 0.7872 - 0.7874 in. per Drawing 4040T20, Zone A7

Hardness Rockwell C 60 to 64 per Drawing 4040T20, Zone C8, Engineering Requirement #13

Internal Clearance per Drawing 4040T20, Zone C8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

83086

99207

New Hampshire Ball Bearings Inc Hitech Div

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axis A Duplex Ball BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

11/26/2009CSI Date

4040T20P03 3110 01 087 - 4284

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter between 0.7872 - 0.7874 in. per Drawing 4040T20, Zone A7

Hardness Rockwell C 60 to 64 per Drawing 4040T20, Zone C8, Engineering Requirement #13

Internal Clearance per Drawing 4040T20, Zone C8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

83086

99207

New Hampshire Ball Bearings Inc Hitech Div

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axis A Duplex Ball BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

11/26/2009CSI Date

4040T21P01 3110 01 087 - 4283

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.9841-0.9843 in. per Drawing 4040T21, Zone A8

Hardness Rockwell C 60 to 64 per Drawing 4040T21, Zone C8, Engineering Requirement #13

Internal Clearance per Drawing 4040T21, Zone C8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

70854

99207

Barden Corporation

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axis B Duplex Ball BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/21/2009CSI Date

4040T21P03 3110 01 087 - 4283

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.9841-0.9843 in. per Drawing 4040T21, Zone A8

Hardness Rockwell C 60 to 64 per Drawing 4040T21, Zone C8, Engineering Requirement #13

Internal Clearance per Drawing 4040T21, Zone C8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

83086

99207

New Hampshire Ball Bearings Inc Hitech Div

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axis B Duplex Ball BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/21/2009CSI Date

4041T49P02 2935 01 083 - 6838

N NN

83259 Parker Hannifin Div Composite Sealing Systems

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal, Cooler, LubeNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

4045T93P01 3110 01 087 - 4250

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.7872-0.7874 in. per Drawing 4045T93, Zone B7

Hardness Rockwell C 60 to 64 per Drawing 4045T93, Zone C8, Engineering Requirement #10

Internal Clearance per Drawing 4045T93, Zone C8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

38443

99207

SKF USA Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axis G Roller BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/20/2009CSI Date

4045T93P02 3110 01 087 - 4250

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.7872-0.7874 in. per Drawing 4045T93, Zone B7

Hardness Rockwell C 60 to 64 per Drawing 4045T93, Zone C8, Engineering Requirement #10

Internal Clearance per Drawing 4045T93, Zone C8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axis G Roller BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/20/2009CSI Date

4046T25G01 2935 01 084 - 2430

N

Y

N

N

Y

N

Pressure Test Per DMWR Requirements

Pressure Test Per Spec M50TF2225

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Cooler Assy, OilNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

10/07/1993CSI Date

4046T25G03 2935 01 244 - 4953

N

Y

N

N

Y

N

Pressure Test Per DMWR Requirements

Pressure Test Per Spec M50TF2225

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Cooler Assy, OilNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

10/01/1987CSI Date

4046T25G06 2935 01 304 - 0929

N

Y

N

N

Y

N

Pressure Test Per DMWR Requirements

Pressure Test Per Spec M50TF2225

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Cooler Assy, OilNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

01/16/1996CSI Date

4046T28G14 2995 01 294 - 9867

N

Y

N

N

Y

N

Acceptance Test per Army DMWR 55-2995-231

OEM Acceptance Test Procedure

1PVC5

99207

Vacco Industries Inc El Segundo Products Div

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Valve Assy, Bleed/StartNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/14/2001CSI Date

4046T28G15 2995 01 313 - 0691

N

Y

N

N

Y

N

Acceptance Test per Army DMWR 55-2995-231

OEM Acceptance Test Procedure

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Valve Assy, Bleed/StartNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/14/2001CSI Date

4053T74P01 5930 01 135 - 0096

N NN

55723

99207

Spectrum Associates Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Switch, Fuel PressureNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

4069T08G01 2995 01 120 - 7538

Y

N

N

Y

N

N

N

N

Y

Y

Y

Y

Contains CSI Subcomponents

Engine Acceptance Test Procedure per DMWR

Pressure test per DMWR

Verification of proper gasket installation is required

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Manifold, PressurizedNoun YCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

10/07/1993CSI Date

4069T34P02 2915 01 141 - 7557

Y

Y

N

N

N

N

N

N

N

Dimension B .509 max, .505 min. circular

Dimension C .326 max, .322 min. circular

Not established as a single component. Buy from approved sources. If other than approved is required, CC will be generated at that time.

98391

99207

Arkwin Industries Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stop, Valve, SelectorNoun YCritical Safety

NSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

05/08/2000CSI Date

4069T46P01 2915 01 140 - 6759

Y

Y

N

N

N

N

Must pass the assembly level Acceptance Test Procedure (ATP)

Not established as a single component. Buy from approved sources. If other than approved is required, CC will be generated at that time.

18350

98391

99207

Pall Aeropower Corp Sub of Pall Corp

Arkwin Industries Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Filter Element, FluidNoun YCritical Safety

NSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

05/08/2000CSI Date

4106T40P06 5340 01 487 - 8361

N NN

70472

77535

99207

Barnes Group Inc

Barnes Group Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal PlateNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

4106T43P01 5360 01 493 - 6801

N NN

30408

99207

Barnes Group Inc Associated Spring Div

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Spring, BearingNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

4106T80P01 2840 01 509 - 0315

N

Y

Y

N

N

N

Y

N

N

Absence of cracks via FPI per DMWR Requirements

Bolt hole dimensions per drawing (Sheet 2, Zones A4, A5 and A6)

FPI per drawing

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 2, Fwd Cooling PlateNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

11/03/2005CSI Date

4903T20P01 3120 01 346 - 3551

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Bushing, FlangedNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

CSI Date

4903T21P01 3120 01 346 - 9151

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Bushing, FlangedNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

CSI Date

4903T21P02 3120 01 347 - 0637

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Bushing, FlangedNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

CSI Date

5034T04P01 3110 01 097 - 2292

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 1.5746 -1.5748 in. per Drawing 5034T04, zone C7

Hardness Rockwell C 60 to 64 per Drawing 5034T04, Zone F8, Engineering Requirement #13

Internal Clearance per Drawing 5034T04, zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

#6 Annular Ball, separableNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/20/2009CSI Date

5034T06P01 3110 01 084 - 2368

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 1.5766 -1.5768 in. per Drawing 5034T06, Zone B7

Hardness Rockwell C 60 to 64 per Drawing 5034T06, Zone F8, Engineering Requirement #12

Internal Clearance per Drawing 5034T06, Zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

38443

99207

SKF USA Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

#5 Roller Bearing, SeparableNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/20/2009CSI Date

5034T07P03 3110 01 084 - 2530

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 2.4014-2.4016 in. per Drawing 5034T07, Zone B7

Hardness Rockwell C 60 to 64 per Drawing 5034T07, Zone F8, Engineering Requirement #13

Internal Clearance per Drawing 5034T07, zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

70854

99207

Barden Corporation

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

#1 Annular Duplex Ball BrngNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/24/2009CSI Date

5034T11P05 4320 01 295 - 1989

N

Y

N

N

Y

N

Acceptance Test Procedures per DMWR 55-2840-252

OEM Acceptance Test Procedures

86329

99207

Parker-Hannifin Corp Nichols Aircraft Div

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Pump, Lubricating & ScavengeNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

03/01/2004CSI Date

5034T19P02 3130 01 087 - 4246

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.7872-0.7874 in. per Drawing 5034T19, Zone C7

Hardness Rockwell C 58-62 per Drawing 5034T19, Zone F8, Engineering Requirement #13.

Internal Clearance per Drawing 5034T19, Zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

38443

99207

SKF USA Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axes C, D, E, F Annular B BgNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/21/2009CSI Date

5034T19P03 3130 01 087 - 4246

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.7872-0.7874 in. per Drawing 5034T19, Zone C7

Hardness Rockwell C 58-62 per Drawing 5034T19, Zone F8, Engineering Requirement #13.

Internal Clearance per Drawing 5034T19, Zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

6T122

99207

Timken US Corporation

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axes C, D, E, F Annular B BgNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/21/2009CSI Date

5034T22P01 3130 01 087 - 4248

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.9841 -0.9843 in. per Drawing 5034T22, Zone D7

Hardness Rockwell C 60 to 64 per Drawing 5034T22, Zone F8, Engineering Requirement #10

Internal Clearance per Drawing 5034T22, Zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

38443

99207

SKF USA Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axes B, E Cyl Roller BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/20/2009CSI Date

5034T22P02 3130 01 087 - 4248

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.9841 -0.9843 in. per Drawing 5034T22, Zone D7

Hardness Rockwell C 60 to 64 per Drawing 5034T22, Zone F8, Engineering Requirement #10

Internal Clearance per Drawing 5034T22, Zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

78118

99207

Timken Aerospace

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axes B, E Cyl Roller BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/20/2009CSI Date

5034T27P01 3110 01 084 - 2368

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 1.5766 -1.5768 in. per Drawing 5034T27, Zone B7

Hardness Rockwell C 60 to 64 per Drawing 5034T27, Zone F8, Engineering Requirement #12

Internal Clearance per Drawing 5034T27, zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

78118

99207

Timken Aerospace

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

# 5 Bearing, RollerNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/20/2009CSI Date

5034T27P02 3110 01 084 - 2368

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 1.5766 -1.5768 in. per Drawing 5034T27, Zone B7

Hardness Rockwell C 60 to 64 per Drawing 5034T27, Zone F8, Engineering Requirement #12

Internal Clearance per Drawing 5034T27, Zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

36069

99207

FAG Bearing Ltd

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

# 5 Bearing, RollerNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

12/22/2009CSI Date

5034T28P01 3110 01 097 - 2292

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 1.5746 -1.5748 in. per Drawing 5034T28, zone C7

Hardness Rockwell C 60 to 64 per Drawing 5034T28, Zone F8, Engineering Requirement #13

Internal Clearance per Drawing 5034T28, zone H8, Engineering Requirements #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

No. 6 Annular Ball BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/20/2009CSI Date

5034T29P01 3130 01 087 - 4249

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.7872 -0.7874 in. per Drawing 5034T29, Zone C7

Hardness Rockwell C 60 to 64 per Drawing 5034T29, Zone F8, Engineering Requirement #10

Internal Clearance per Drawing 5034T29, Zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

38443

99207

SKF USA Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axes A, C, D, and F Roll BrgNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/20/2009CSI Date

5034T29P02 3130 01 087 - 4249

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.7872 -0.7874 in. per Drawing 5034T29, Zone C7

Hardness Rockwell C 60 to 64 per Drawing 5034T29, Zone F8, Engineering Requirement #10

Internal Clearance per Drawing5034T29, Zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

78118

99207

Timken Aerospace

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axes A, C, D, and F Roll BrgNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/20/2009CSI Date

5034T31P01 2935 01 108 - 2801

N

Y

N

N

Y

N

Pressure Test Per DMWR Requirements

Pressure Test Per Spec M50TF2225

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Cooler, Lube OilNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

10/07/1993CSI Date

5034T31P02 2935 01 328 - 7261

N

Y

N

N

Y

N

Pressure Test Per DMWR Requirements

Pressure Test Per Spec M50TF2225

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Cooler, Lube OilNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

01/16/1996CSI Date

5034T51P01 3130 01 087 - 4247

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.7872-0.7874 in. per Drawing 5034T51, Zone C7

Hardness Rockwell C 60 to 64 per Drawing 5034T51, Zone F6, Engineering Requirement #13

Internal Clearance per Drawing 5034T51, Zone H6, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

38443

99207

SKF USA Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axis G Annular Ball BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

10/19/2011CSI Date

5034T51P02 3130 01 087 - 4247

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.7872-0.7874 in. per Drawing 5034T51, Zone C7

Hardness Rockwell C 60 to 64 per Drawing 5034T51, Zone F6, Engineering Requirement #13

Internal Clearance per Drawing 5034T51, Zone H6, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

6T122

99207

Timken US Corporation

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axis G Annular Ball BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

10/19/2011CSI Date

5034T69P01 3040 01 089 - 0995

Y

Y

Y

Y

N

N

N

N

N

N

N

N

N

N

Y

Hardness Requirements (per note 5 of drawing 5034T69)

Heat Treat requirements (per note 13 of drawing 5034T69)

Magnetic Particle inspection (per note 6 of drawing 5034T69)

Nital Etch (per drawing 5034T69), zone B2

Visual Inspection for cracks

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Gearshaft, SpurNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

11/05/2009CSI Date

5034T73P01 3020 01 091 - 4827

Y

Y

Y

Y

N

N

N

N

N

N

N

N

N

N

Y

Hardness Requirements (per note 5 of drawing 5034T73)

Heat Treat requirements (per note 13 of drawing 5034T73)

Magnetic Particle inspection (per note 6 of drawing 5034T73)

Nital Etch (per drawing 5034T73), zone B2

Visual Inspection for cracks

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Gear, SpurNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

10/19/2011CSI Date

5034T75P01 3020 01 097 - 9786

Y

Y

Y

Y

N

N

N

N

N

N

N

N

N

N

Y

Hardness Requirements (per note 5 of drawing 5034T75)

Heat Treat requirements (per note 13 of drawing 5034T75)

Magnetic Particle inspection (per note 6 of drawing 5034T75)

Nital Etch (per drawing 5034T75), zone B2

Visual Inspection for cracks

21540

57152

99207

Precision Gear Inc

Triumph Gear Systems

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Gear, SpurNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

04/01/1987CSI Date

5034T77P01 3040 01 088 - 1924

N NN

21540

99207

A3460

Precision Gear Inc

General Electric Company (Aircraft Engine Business Group)

AVIO SPA

CAGE

Critical CharacteristicsM ID

Part No NSN

Shaft, ShoulderedNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

5034T78P01 3020 01 091 - 4826

Y

Y

Y

Y

N

N

N

N

N

N

N

N

N

N

Y

Hardness requirements per Drawing 5034T78, Note 5.A to 5.E and 5.G to 5.K

Heat Treat requirements (per note 13 of drawing 5034T78)

Magnetic Particle inspection (per note 6 of drawing 5034T78)

Nital Etch (per drawing 5034T78), zone B2

Visual Inspection for cracks

21540

99207

Precision Gear Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Gear, SpurNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

04/01/1987CSI Date

5034T79P01 3020 01 097 - 0904

N NN

99207

A3460

General Electric Company (Aircraft Engine Business Group)

AVIO SPA

CAGE

Critical CharacteristicsM ID

Part No NSN

Gear, BevelNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

CSI Date

5034T80P01 3040 01 087 - 4276

N NN

21540

99207

Precision Gear Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shaft, ShoulderedNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

5034T91P06 2915 01 089 - 9265

N

Y

Y

N

N

N

Y

N

N

Acceptance Test per Army DMWR 55-2915-341

Acceptance Test per drawing (G.E. design specification AMC-CE-2222-02010)

Spline data per note 4 and table (zone G-8 & H-8) of drawing 5034T91; as measured or as verified by spline gauges

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Pump, Fuel BoostNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

07/18/1996CSI Date

5035T69P01 3110 01 089 - 4209

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 1.5698 -1.5700 in. per Drawing 5035T69, Zone B7

Hardness Rockwell C 60 to 64 per Drawing 5035T69, Zone F8, Engineering Requirement #12

Internal Clearance per Drawing 5035T69, Zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

78118

99207

Timken Aerospace

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

No. 2 Trilobe Roller BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

11/14/2001CSI Date

5035T69P02 3110 01 089 - 4209

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 1.5698 -1.5700 in. per Drawing 5035T69, Zone B7

Hardness Rockwell C 60 to 64 per Drawing 5035T69, Zone F8, Engineering Requirement #12

Internal Clearance per Drawing 5035T69, Zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

36069 FAG Bearing Ltd

CAGE

Critical CharacteristicsM ID

Part No NSN

No. 2 Trilobe Roller BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

11/15/2001CSI Date

5035T71P01 3110 01 087 - 4251

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 1.5698 -1.5700 in. per Drawing 5035T71, Zone C7

Hardness Rockwell C 60 to 64 per Drawing 5035T71, Zone F8, Engineering Requirement #12

Internal Clearance per Drawing 5035T71, Zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

No. 2 Trilobe Roller BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/24/2009CSI Date

5035T82P01 3040 01 087 - 4275

N NN

57152

99207

A3460

Triumph Gear Systems

General Electric Company (Aircraft Engine Business Group)

AVIO SPA

CAGE

Critical CharacteristicsM ID

Part No NSN

Shaft, ShoulderedNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

5036T84P01 3020 01 098 - 7608

Y

Y

Y

Y

N

N

N

N

N

N

N

N

N

N

Y

Hardness Requirements (per note 5 of drawing 5036T84)

Heat Treat requirements (per note 10 of drawing 5036T84)

Magnetic Particle inspection (per note 6 of drawing 5036T84)

Nital Etch (per drawing 5036T84), zone B2

Visual Inspection for cracks

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Gear, SpurNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

10/11/2001CSI Date

5043T07G02 5310 01 280 - 9848

N NN

07039

99207

Berkshire Industries Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Nut, Tie-Rod CompressionNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

5043T18P01 3110 01 084 - 2530

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 2.4014-2.4016 in. per Drawing 5043T18, Zone C8

Hardness Rockwell C 60 to 64 per Drawing 5043T18, Zone F8, Engineering Requirement #13

Internal Clearance per Drawing 5043T18, Zone H8, Engineering Requirement #2

MPI or FPI per M50TF5 CL-A; Para. 4.2.2 Magnetic Particle Inspection and Table 1 or Para. 4.2.3 Fluorescent Penetration Inspection Maximum Permissible Surface Conditions for Balls, Roller, Raceways per M50TF5 CL-A; Table II

Nital etch inspection per M50TF5 CL-A; Para. 4.2.7.1 Nital Etch Requirements

38443

99207

SKF USA Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

#1 Bearing, Ball DuplexNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/25/2009CSI Date

5043T75G33 -

Y NY Item contains CSI items

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Power Turbine Rotor AssyNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

11/03/2005CSI Date

5044T07P01 2840 01 089 - 4127

N NN

07039

0TA23

99207

Berkshire Industries Inc

New England Carbide Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal, AirNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

5044T08P10 2995 01 294 - 9867

N

Y

N

N

Y

N

Acceptance Test per Army DMWR 55-2995-231

OEM Acceptance Test Procedure

1PVC5

99207

Vacco Industries Inc El Segundo Products Div

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Valve, A/I Bleed & StartNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/14/2002CSI Date

5044T08P11 2995 01 313 - 0691

N

Y

N

N

Y

N

Acceptance Test per Army DMWR 55-2995-231

OEM Acceptance Test Procedure

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Valve Assy, Bleed/StartNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

08/14/2002CSI Date

5044T18G01 2840 01 087 - 1695

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal, AirNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

5044T23G01 2840 01 102 - 3022

N NN

57488

98839

99207

LKM Industries Inc

Hansen Engineering and Machinery Company Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal, AirNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

5044T27G02 3010 01 235 - 7917

N YN Installation of damping ring

36480 Northstar Aerospace (Canada) Inc.

CAGE

Critical CharacteristicsM ID

Part No NSN

Drive Assy, PowerNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

03/24/1992CSI Date

5044T94G01 2840 01 140 - 6732

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Duct, Anti-Icing InletNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

5044T95G01 4710 01 141 - 7558

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Tube, Feed, Guide VaneNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

5051T18G01 -

Y

Y

Y

N

N

N

N

N

N

Braze per drawing note 7

FPI per drawing note 8

Pressure test per drawing note 3

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Manifold, Overspeed & DrainNoun YCritical Safety

NSerial Number Req'd NEngineering Test Req'd NFatigue NEndurance NInterchange

Approved Replacement (Spares) Sources

01/13/2010CSI Date

5056T27G02 2840 01 249 - 1072

N NN

50554

99207

Metro Machine Works Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal, AirNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

CSI Date

5056T66G02 3010 01 317 - 3481

Y

N

N

Y

Y

N

Assembly contains Critical Safety Items

Installation of Damping Ring

57152

99207

Triumph Gear Systems

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Drive Assy, PowerNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

03/01/1994CSI Date

5057T06P01 3110 01 287 - 9655

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.7872-0.7874 in. per Drawing 5057T06, Zone D7

Hardness Rockwell C 61 to 65 per Drawing 5057T06 , Zone F8, Engineering Requirement #11

Internal Clearance per Drawing 5057T06, Zone H8, Engineering Requirement #2

Magnetic Particle Inspection per M50TF32 CL-A, Para. 4.1.2.1.8; per P29TF39 CL-A, Para. 3.2.2.4.3 Magnetic Particle Acceptability Limits, Table IV, Allowable Indications Maximum Permissible Surface Conditions for Balls, Roller, Raceways per P29TF39 CL-A; Table II

Nital etch inspection per M50TF32 CL-A; Para. 4.1.6.1 Overheating

38443

99207

SKF USA Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axis G Bearing, Roll, CylNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

10/19/2011CSI Date

5057T06P03 3110 01 287 - 9655

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.7872-0.7874 in. per Drawing 5057T06, Zone D7

Hardness Rockwell C 61 to 65 per Drawing 5057T06 , Zone F8, Engineering Requirement #11

Internal Clearance per Drawing 5057T06, Zone H8, Engineering Requirement #2

Magnetic Particle Inspection per M50TF32 CL-A, Para. 4.1.2.1.8; per P29TF39 CL-A, Para. 3.2.2.4.3 Magnetic Particle Acceptability Limits, Table IV, Allowable Indications Maximum Permissible Surface Conditions for Balls, Roller, Raceways per P29TF39 CL-A; Table II

Nital etch inspection per M50TF32 CL-A; Para. 4.1.6.1 Overheating

78118

99207

Timken Aerospace

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axis G Bearing, Roll, CylNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

10/19/2011CSI Date

5057T58P02 3110 01 302 - 9262

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.7872 -0.7874 in. per Drawing 5034T58, Zone D7

Hardness Rockwell C 61 to 65 per Drawing 5057T58 , Zone F8, Engineering Requirement #11

Internal Clearance per Drawing 5057T58, Zone H8, Engineering Requirement #2

Magnetic Particle Inspection per M50TF32 CL-A, Para. 4.1.2.1.8; per P29TF39 CL-A, Para. 3.2.2.4.3 Magnetic Particle Acceptability Limits, Table IV, Allowable Indications Maximum Permissible Surface Conditions for Balls, Roller, Raceways per P29TF39 CL-A; Table II

Nital etch inspection per M50TF32 CL-A; Para. 4.1.6.1 Overheating

06144

99207

Industrial Tectonics Bearings Corporation

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axes A, C, D, & F Roller BrgNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

10/19/2011CSI Date

5057T58P03 3110 01 302 - 9262

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.7872 -0.7874 in. per Drawing 5034T58, Zone D7

Hardness Rockwell C 61 to 65 per Drawing 5057T58 , Zone F8, Engineering Requirement #11

Internal Clearance per Drawing 5057T58, Zone H8, Engineering Requirement #2

Magnetic Particle Inspection per M50TF32 CL-A, Para. 4.1.2.1.8; per P29TF39 CL-A, Para. 3.2.2.4.3 Magnetic Particle Acceptability Limits, Table IV, Allowable Indications Maximum Permissible Surface Conditions for Balls, Roller, Raceways per P29TF39 CL-A; Table II

Nital etch inspection per M50TF32 CL-A; Para. 4.1.6.1 Overheating

78118

99207

Timken Aerospace

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axes A, C, D, & F Roller BrgNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

10/19/2011CSI Date

5057T59P01 3110 01 302 - 9263

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.9841 -0.9843 in per Drawing 5057T59, Zone C7

Hardness Rockwell C 61 to 65 per Drawing 5057T59 , Zone F8, Engineering Requirement #11

Internal Clearance per Drawing 5057T59, Zone H8, Engineering Requirement #2

Magnetic Particle Inspection per M50TF32 CL-A, Para. 4.1.2.1.8; per P29TF39 CL-A, Para. 3.2.2.4.3 Magnetic Particle Acceptability Limits, Table IV, Allowable Indications Maximum Permissible Surface Conditions for Balls, Roller, Raceways per P29TF39 CL-A; Table II

Nital etch inspection per M50TF32 CL-A; Para. 4.1.6.1 Overheating

38443

99207

SKF USA Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axes B, E Roller BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

10/19/2011CSI Date

5057T59P03 3110 01 302 - 9263

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

N

N

N

N

N

Bore Diameter per Engine DMWR

Bore diameter 0.9841 -0.9843 in per Drawing 5057T59, Zone C7

Hardness Rockwell C 61 to 65 per Drawing 5057T59 , Zone F8, Engineering Requirement #11, Internal Clearance per Drawing 5057T59, zone H8, Engineering Requirement #2

Magnetic Particle Inspection per M50TF32 CL-A, Para. 4.1.2.1.8; per P29TF39 CL-A, Para. 3.2.2.4.3 Magnetic Particle Acceptability Limits, Table IV, Allowable Indications Maximum Permissible Surface Conditions for Balls, Roller, Raceways per P29TF39 CL-A; Table II

Nital etch inspection per M50TF32 CL-A; Para. 4.1.6.1 Overheating

78118

99207

Timken Aerospace

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Axes B, E Roller BearingNoun YCritical Safety

YSerial Number Req'd YEngineering Test Req'd YFatigue YEndurance YInterchange

Approved Replacement (Spares) Sources

10/19/2011CSI Date

5060T51G01 2840 01 385 - 1157

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal, Metallic, SpecialNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

5060T51G03 2840 01 385 - 1157

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal, Metallic, SpecialNoun NCritical Safety

NSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

5066T16G25 2840 01 509 - 0308

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Segment Assy, Stage 2 NozzleNoun NCritical Safety

YSerial Number Req'd YEngineering Test Req'd NFatigue YEndurance NInterchange

Approved Replacement (Spares) Sources

CSI Date

5066T38G04…