Attachment_0038_Critical_Characteristics.pdf

PDF 64 KB Posted

Attached to
Solicitation Amendment For the Overhaul/Upgrade of the UH-60 Power Turbine
Solicitation number
W58RGZ-19-R-0081
Issued by

About this file

Written by GovTribe AI ·

This document provides critical characteristics and specifications for aircraft engine parts. It lists over 70 part numbers with details including required tests, inspections, dimensions and material properties. The parts include bearings, seals, shafts, discs, blades and other turbine components. Testing and inspection requirements include magnetic particle inspection, fluorescent penetrant inspection, hardness testing, ultrasonic inspection and absence of cracks. The related federal contract opportunity is a solicitation amendment for the overhaul and upgrade of the UH-60 power turbine issued by the Department of the Army Materiel Command Contracting Command Redstone Arsenal. It seeks services but provides no further description. The document primarily provides technical specifications for aircraft engine components rather than directly addressing a federal contract.

From the source

Attachment 0038_Critical Characteristics.pdf

View the file

Other files

File Type Posted
W58RGZ-19-R-0081_0003.pdf PDF
W58RGZ19R0081-0002.pdf PDF
W58RGZ19R0081-0001.pdf PDF
Attachment_0043_Document_Summary_List.pdf PDF
Attachment_0040_Frozen_Plan_Description_and_Guidance.pdf PDF
Attachment_0042_Depot_Maintenance_Production_Report_Sample.xlsx XLSX spreadsheet
Attachment_0041_DD_Form_1348-1A_Example.pdf PDF
Exhibit_B_Data_Item_A002.pdf PDF
Exhibit_D_Data_Item_A004.pdf PDF
Exhibit_E_Data_Item_A005.pdf PDF
Attachment_0044_Packaging_Requirements.pdf PDF
Exhibit_A_Data_Item_A001.pdf PDF
Exhibit_F_Data_Item_A006.pdf PDF
Attachment_0045_TDPL.pdf PDF
Exhibit_C_Data_Item_A003.pdf PDF
Attachment_0039_Report_of_Discrepancy_Guidance.pdf PDF
W58RGZ-19-R-0081.pdf PDF
Show all 17

On GovTribe

Work with this file

  • Download the original file
  • Contacts named in this file
  • Similar government files
  • Ask GovTribe AI about this file
Try for free Login

Text version

The file's text, extracted by GovTribe without its formatting.

03/14/2017

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

Approved Date

M&O CRITICAL SAFETY ITEMS

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

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. 4.2.2 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

# 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

5043T75G15 2840 01 281 - 3581

Y NY Item contains CSI items

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Rotor, Power TurbineNoun YCritical Safety

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

Approved Replacement (Spares) Sources

02/09/2009CSI 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

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

5088T39G04 2840 01 425 - 5361

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shroud Segment Assy, TurbineNoun NCritical Safety

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

Approved Replacement (Spares) Sources

CSI Date

5125T91P01 2840 01 514 - 1102

Y

N

N

N

N

Y

FPI per Drawing 5125T91 note 4

FPI verification that cracks are within DMWR limits

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shaft,Turbine,Aircraft GasNoun YCritical Safety

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

Approved Replacement (Spares) Sources

07/01/2010CSI Date

5125T91P01RE -

N NY FPI verification that cracks are within DMWR limits

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shaft,Turbine,Aircraft GasNoun YCritical Safety

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

Approved Replacement (Spares) Sources

07/01/2010CSI Date

5125T92G01 2840 01 473 - 3556

Y

Y

N

N

N

N

N

N

N

Y

Y

Y

Absence of cracks via fluorescent penetrant inspection per drawing note 5

Assembly contains CSI sub-components

White Light Inspection verification of an absence of cracks after balance grinding.

White light inspection verification of an absence of cracks for, complete shaft assemblies with 150 or less operating hours since last full inspection and assembly.

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shaft Assy, Power TurbineNoun YCritical Safety

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

Approved Replacement (Spares) Sources

08/13/2001CSI Date

5125T92G01RE 2840 01 473 - 3556

Y

N

N

N

N

N

Y

Y

Y

Assembly contains CSI sub-components

White Light Inspection verification of an absence of cracks after balance grinding.

White light inspection verification of an absence of cracks for complete shaft assemblies with 150 or less operating hours since last full inspection and assembly.

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shaft Assy, Power TurbineNoun YCritical Safety

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

Approved Replacement (Spares) Sources

07/01/2010CSI Date

5901T09P01 2840 01 353 - 4540

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal, HoneycombNoun NCritical Safety

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

Approved Replacement (Spares) Sources

CSI Date

6038T32P01 2840 01 082 - 8365

N

N

Y

N

Y

Y

Y

N

N

N

N

N

N

N

Y

Y

N

Y

N

N

N

Absence of cracks via FPI per DMWR requirements; except following a balance grind operation

Absence of cracks via White Light Inspection per DMWR requirements; following a balance grind operation

Absence of cracks via fluorescent penetrant inspection per drawing note 3

Diameter E per DMWR Limits

Hardness on raw material forging drwg (see zone A4 of drwg for forging)

Non-conventional machining material removal, no recast layer allowed, no intergranular attack allowed, no cracks allowed, per note 6 of drawing Results of ultrasonic inspection of forging (see zone A4 of drwg for forging)

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Disc, Turbine, Stage 3Noun YCritical Safety

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

Approved Replacement (Spares) Sources

04/01/1987CSI Date

6038T32P02 2840 01 517 - 5432

N

N

Y

N

Y

Y

Y

Y

N

N

N

N

N

N

N

N

Y

Y

N

Y

N

N

N

N

Absence of cracks via FPI per DMWR requirements; except following a balance grind operation

Absence of cracks via White Light Inspection per DMWR requirements; following a balance grind operation

Absence of cracks via fluorescent penetrant inspection per drawing note 3

Diameter E per DMWR Limits

Hardness of raw material forging drwg (see Zone A4 of drawing for forging)

Non-conventional machining material removal, no recast layer allowed, no intergranular attack allowed, no cracks allowed, per note 6 of drwg Results of ultrasonic inspection of forging (see Zone A4 of drwg for forging)

Shot peen per note 18 of drwg

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Disc, Turbine, Stage 3Noun YCritical Safety

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

Approved Replacement (Spares) Sources

03/30/2005CSI Date

6038T33G02 2840 01 087 - 4207

N NN

50554

99207

Metro Machine Works Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shroud Sector, TurbineNoun NCritical Safety

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

Approved Replacement (Spares) Sources

CSI Date

6038T34P02 2840 01 083 - 3167

N

Y

N

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

Y

N

Y

N

N

Absence of cracks via FPI per DMWR requirements; except following a balance grind operation

Absence of cracks via FPI per drawing note 3

Absence of cracks via White Light Inspection per DMWR requirements; following a balance grind operation

Contour limits of dovetail slots are to be met on all surfaces on both sides of slot simultaneously

Diameter "H"

Hardness

Ultrasonic Inspection of forgings per note 21

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Disc, Turbine, Stage 4Noun YCritical Safety

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

Approved Replacement (Spares) Sources

10/07/1993CSI Date

6038T34P03 2840 01 200 - 9761

N

Y

N

Y

Y

Y

Y

N

N

N

N

N

N

N

Y

N

Y

N

Y

N

N

Absence of cracks via FPI per DMWR requirements; except following a balance grind operation

Absence of cracks via FPI per drawing note 3

Absence of cracks via White Light Inspection per DMWR requirements; following a balance grind operation

Contour limits of dovetail slots are to be met on all surfaces on both sides of slot simultaneously

Diameter "H"

Hardness

Ultrasonic Inspection of forgings per note 21

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Disc, Turbine, Stage 4Noun YCritical Safety

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

Approved Replacement (Spares) Sources

10/07/1993CSI Date

6038T34P05 2840 01 287 - 9668

N

N

Y

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

N

Y

Y

N

Y

N

N

N

N

Absence of cracks via FPI per DMWR requirements; except following a balance grind operation

Absence of cracks via White Light Inspection per DMWR requirements; following a balance grind operation

Contour limits of dovetail slots are to be met on all surfaces on both sides of slot simultaneously

Diameter "H"

Fluorescent penetrant inspection

Hardness

Shot peening per note 26 of drwg

Ultrasonic Inspection of forgings per note 21

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Disc, Turbine, Stage 4Noun YCritical Safety

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

Approved Replacement (Spares) Sources

04/01/1987CSI Date

6038T34P06 2840 01 517 - 5429

N

Y

N

Y

Y

Y

Y

Y

N

N

N

N

N

N

N

N

Y

N

Y

N

Y

N

N

N

Absence of cracks via FPI per DMWR requirements; except following a balance grind operation

Absence of cracks via FPI per drawing note 3

Absence of cracks via White Light Inspection per DMWR requirements; following a balance grind operation

Contour limits of dovetail slots are to be met on all surfaces on both sides of slot simultaneously

Diameter "H"

Hardness

Shot peening per note 26 of drwg

Ultrasonic Inspection of forgings per note 21

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Disc, Turbine, Stage 4Noun YCritical Safety

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

Approved Replacement (Spares) Sources

03/30/2005CSI Date

6038T35G02 2840 01 184 - 7502

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shroud Sector Assy, TurbineNoun NCritical Safety

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

Approved Replacement (Spares) Sources

CSI Date

6038T37G01 2840 01 087 - 4299

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal & Nozzle AssyNoun NCritical Safety

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

Approved Replacement (Spares) Sources

CSI Date

6038T37G02 2840 01 242 - 1758

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal & Nozzle AssyNoun NCritical Safety

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

Approved Replacement (Spares) Sources

CSI Date

6038T37G07 2840 01 419 - 2224

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal & Nozzle AssyNoun NCritical Safety

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

Approved Replacement (Spares) Sources

CSI Date

6038T39P02 2840 01 087 - 4290

N

Y

Y

N

N

N

Y

N

N

Absence of cracks via White Light per DMWR requirements on Coated parts, Absence of cracks via FPI per DMWR requirements on uncoated parts Dovetail contour per drawing note 10

FPI and Visual Inspection Prior to Coating Per Drawing Note 20

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 3 Turbine BladeNoun YCritical Safety

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

Approved Replacement (Spares) Sources

11/30/2005CSI Date

6038T39P08 2840 01 281 - 3611

N

Y

Y

N

N

N

Y

N

N

Absence of cracks via White Light per DMWR requirements on Coated parts, Absence of cracks via FPI per DMWR requirements on uncoated parts Dovetail contour per drawing note 10

FPI and Visual Inspection Prior to Coating Per Drawing Note 20

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 3 Turbine BladeNoun YCritical Safety

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

Approved Replacement (Spares) Sources

11/30/2005CSI Date

6038T39P09 2840 01 493 - 9821

N

Y

Y

N

N

N

Y

N

N

Absence of cracks via White Light per DMWR requirements

Dovetail contour per drawing Note 10

FPI and Visual Inspection Prior to Coating Per Drawing Note 20

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Stage 3 Turbine BladeNoun YCritical Safety

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

Approved Replacement (Spares) Sources

11/03/2005CSI Date

6038T41P02 2840 01 087 - 4291

N

Y

Y

N

N

N

Y

N

N

Absence of cracks via FPI per DMWR requirements

Dovetail Contour per Drawing Note Zone C6

FPI and Visual Inspection Per Drawing Note 16

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Blade, TurbineNoun YCritical Safety

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

Approved Replacement (Spares) Sources

11/30/2005CSI Date

6039T12P01 3130 01 089 - 4120

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Bearing, SupportNoun NCritical Safety

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

Approved Replacement (Spares) Sources

CSI Date

6039T12P02 3130 01 221 - 6025

N NN

06320

2V343

99207

The Pye and Hogan Machine Company

Apex Manufacturing Company Inc

General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Bearing, SupportNoun NCritical Safety

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

Approved Replacement (Spares) Sources

CSI Date

6043T34P01 2840 01 514 - 1102

Y

N

N

N

N

Y

FPI per Drawing 6043T34 note 4

FPI verification that cracks are within DMWR limits.

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shaft,Turbine,Aircraft GasNoun YCritical Safety

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

Approved Replacement (Spares) Sources

07/01/2010CSI Date

6043T35G01 2840 01 102 - 6090

Y

N

N

N

N

N

Y

Y

Y

Assembly contains CSI sub-components

White Light Inspection verification of an absence of cracks after balance grinding.

White light inspection verification of an absence of cracks for complete shaft assemblies with 150 or less operating hours since last full inspection and assembly.

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shaft Assy, DriveNoun YCritical Safety

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

Approved Replacement (Spares) Sources

04/01/1987CSI Date

6055T07G01 2840 01 247 - 9514

N NN

99207

A3344

General Electric Company (Aircraft Engine Business Group)

Alfa Romeo Avio Spa

CAGE

Critical CharacteristicsM ID

Part No NSN

Seal, Stationary, AirNoun NCritical Safety

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

Approved Replacement (Spares) Sources

CSI Date

6058T13G11 2840 01 362 - 4935

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Nozzle Duct & Air Seal AssyNoun NCritical Safety

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

Approved Replacement (Spares) Sources

CSI Date

6064T36P01 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 6064T36, Zone B11

Hardness Rockwell C 60 to 64 per Drawing 6064T36, Zone F12, Engineering Requirement #13

Internal Clearance per Drawing 6064T36, Zone H12, 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

#6 Annular Ball, SeparableNoun YCritical Safety

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

Approved Replacement (Spares) Sources

10/28/2013CSI Date

6064T36P02 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 6064T36, Zone B11

Hardness Rockwell C 60 to 64 per Drawing 6064T36, Zone F12, Engineering Requirement #13

Internal Clearance per Drawing 6064T36, Zone H12, 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

36069

99207

FAG Bearing Ltd

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

10/28/2013CSI Date

6064T37P01 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 6064T37, zone B11

Hardness Rockwell C 60 to 64 per Drawing 6064T37, Zone F12, Engineering Requirement #13

Internal Clearance per Drawing 6064T37, zone H12, 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; Para 3.2.2.4.1.1, 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

No. 6 Annular BallNoun YCritical Safety

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

Approved Replacement (Spares) Sources

08/27/2010CSI Date

6064T80P01 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 6064T80, Zone B10

Hardness Rockwell C 60 to 64 per Drawing 6064T80 , Zone F12, Engineering Requirement #12

Internal Clearance per Drawing 6064T80, Zone H12, 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

# 5 Bearing, RollerNoun YCritical Safety

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

Approved Replacement (Spares) Sources

08/20/2009CSI Date

6071T26G02 2840 01 503 - 1700

Y

Y

N

Y

Y

Y

Assembly contains CSI items

Installation of stage 4 Turbine Stator Ring

062W2

24113

3AH19

S0204

GE Engine Services Inc

GE Engine Services Inc DBA GE

Vector Aerospace

Bet Shemesh Engines Inc

CAGE

Critical CharacteristicsM ID

Part No NSN

Module Assy, Power TurbineNoun YCritical Safety

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

Approved M&O Sources

11/03/2005CSI Date

6071T80G03 2840 01 342 - 5949

N NN

99207 General Electric Company (Aircraft Engine Business Group)

CAGE

Critical CharacteristicsM ID

Part No NSN

Shroud Segment Assy, TurbineNoun NCritical Safety

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

Approved Replacement (Spares) Sources

CSI Date

File details come from the government source that posted it. Updated .