Atachment 0006 - MO Critital Safety Items _T359.pdf
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- Attached to
- Overhaul of the UH-60 POWER TURBINE MODULE
- Solicitation number
- W58RGZ-26-B-0012
About this file
This document is a Maintenance and Operations (M&O) Critical Safety Items list for the T701D engine used in the UH-60L/AH-64A helicopter systems. It identifies 47 parts designated as critical safety items requiring specific inspection, testing, and quality control requirements to ensure airworthiness and operational safety.
The document specifies detailed critical characteristics for each part, including dimensional tolerances, material specifications, inspection methods (such as fluorescent penetrant inspection, ultrasonic inspection, and white light inspection), hardness requirements, and surface condition standards. Key component categories include bearings (annular ball and roller types), turbine discs and blades (stages 3 and 4), turbine shafts and rotors, seals, nozzle assemblies, bushings, and shroud segments. Each part entry includes the part number, National Stock Number (NSN), nomenclature, Critical Safety Item (CSI) certification date, serial number requirements, engineering test requirements, fatigue and endurance testing requirements, and approved replacement sources identified by CAGE codes. General Electric Company (Aircraft Engine Business Group) is listed as the primary or sole approved source for maintenance and overhaul on all items; secondary approved sources such as SKF USA Inc, Timken Aerospace, Schaeffler Aerospace Canada Inc, and others are identified for specific bearing and component replacements. The list establishes mandatory production and quality standards ensuring that all critical safety components meet rigorous engineering specifications before installation or use in military helicopter power plant systems.
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M&O Critical Safety Items
Part Number
Yes - 1/15/2021Nomenclature
NSN6071T26G05
CSI /
Date
MODULE ASSY, POWER TURBINE
2840-01-692-2620
M D I Critical Characteristic
Y Y Y Installation of stage 4 Turbine Stator Ring.
Y Y N Assembly contains CSI items.
CAGE Approved Replacement (Spares) Source Name
L0K02 Standard Aero Limited
24113 GE Engine Services Inc DBA GE
1855A Bet Shemesh Engine LTD.
062W2 GE Engine Services Inc
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes No Yes No
Output Part
Part Number
Yes - 8/20/2009Nomenclature
NSN5034T04P01
CSI /
Date
#6 Annular Ball, separable
3110-01-097-2292
M D I Critical Characteristic
Y N N Outer Ring OD 3.3462 - 3.3465 in. per Drawing 5034T04, Zone C8.
Y N N Radial Internal Clearance .0036 - .0054 in. per Drawing 5034T04, Zone H8, Engineering Requirement #2.
Y N N Maximum Permissible Surface Condition for Balls, Rollers, Raceways per M50TF5 CL-A Table II.
Y N N MPI Limits per M50TF5 CL-A, Para. 4.2.2, Table 1 (allowable indications).
Y N N Nital Etch Inspection M50TF5 CL-A, Para. 4.2.7.1, Overheating.
Y N N Hardness Rockwell C 60 to 64 per Drawing 5034T04, Zone F8, Engineering Requirement #13.
Y N N Bore Diameter 1 .5746 - 1.5748 in. per Drawing 5034T04, Zone D7.
N Y N Radial Internal Clearance per Engine DMWR.
N Y N Outside Diameter per Engine DMWR.
N Y N Bore Diameter per Engine DMWR.
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes Yes Yes Yes
PRI
D
T359 Part Number
NomenclatureNSN System
Status6071T26G05
MODULE ASSY, POWER TURBINE2840-01-692-2620 UH–60L/AH–
64A ENGINE
(T701D)
Routine
Page 1 of 15M&O Critical Safety Items - T359
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Part Number
Yes - 8/20/2009Nomenclature
NSN5034T06P01
CSI /
Date
#5 Roller Bearing, Separable
3110-01-084-2368
M D I Critical Characteristic
Y N N Outer Ring OD 2.6769 - 2.6772 in. per Drawing 5034T06, Zone C6.
Y N N Radial Internal Clearance .0010 - .0014 in. per Drawing 5034T06, Zone H8, Engineering Requirement #2.
Y N N Maximum Permissible Surface Condition for Balls, Rollers, Raceways per M50TF5 CL-A Table II.
Y N N MPI Limits per M50TF5 CL-A, Para. 4.2.2, Table I (allowable indications).
Y N N Nital Etch Inspection M50TF5 CL-A, Para. 4.2.7.1, Overheating.
Y N N Hardness Rockwell C 60 - 64 per drawing 5034T06, Zone F8, Engineering Requirement #12.
Y N N Inner Ring Bore Diameter 1.5766 - 1.5768 in. per Drawing 5034T06, Zone B7.
N Y N Radial Internal Clearance per Engine DMWR.
N Y N Outside Diameter per Engine DMWR.
N Y N Bore Diameter per Engine DMWR.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
38443 SKF USA Inc
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes Yes Yes Yes
Part Number
Yes - 8/20/2009Nomenclature
NSN5034T27P01
CSI /
Date
# 5 Bearing, Roller
3110-01-084-2368
M D I Critical Characteristic
Y N N Outer Ring OD 2.6769 - 2.6772 in. per Drawing 5034T27, Zone C6.
Y N N Radial Internal Clearance .0010 - .0014 in. per Drawing 5034T27, Zone H8, Engineering Requirement #2.
Y N N Maximum Permissible Surface Condition for Balls, Rollers, Raceways per M50TF5 CL-A Table II.
Y N N MPI Limits per M50TF5 CL-A, Para. 4.2.2, Table I (allowable indications).
Y N N Nital Etch Inspection M50TF5 CL-A, Para. 4.2.7.1, Overheating.
Y N N Hardness Rockwell C 60 - 64 per Drawing 5034T06, Zone F8, Engineering Requirement #12.
Y N N Inner Ring Bore Diameter 1.5766 - 1.5768 in. per Drawing 5034T27, Zone B7.
N Y N Radial Internal Clearance per Engine DMWR.
N Y N Outside Diameter per Engine DMWR.
N Y N Bore Diameter per Engine DMWR.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes Yes Yes Yes
Page 2 of 15M&O Critical Safety Items - T359
78118 Timken Aerospace
Yes - 12/22/2009Nomenclature
NSN5034T27P02
CSI /
Date
# 5 Bearing, Roller
3110-01-084-2368
M D I Critical Characteristic
Y N N Outer Ring OD 2.6769 - 2.6772 in. per Drawing 5034T27, Zone C6.
Y N N Radial Internal Clearance .0010 - .0014 in. per Drawing 5034T27, Zone H8, Engineering Requirement #2.
Y N N Maximum Permissible Surface Condition for Balls, Rollers, Raceways per M50TF5 CL-A Table II.
Y N N MPI Limits per M50TF5 CL-A, Para. 4.2.2, Table I (allowable indications).
Y N N Nital Etch Inspection M50TF5 CL-A, Para. 4.2.7.1, Overheating.
Y N N Hardness Rockwell C 60 - 64 per Drawing 5034T06, Zone F8, Engineering Requirement #12.
Y N N Inner Ring Bore Diameter 1.5766 - 1.5768 in. per Drawing 5034T27, Zone B7.
N Y N Radial Internal Clearance per Engine DMWR.
N Y N Outside Diameter per Engine DMWR.
N Y N Bore Diameter per Engine DMWR.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
36069 Schaeffler Aerospace Canada Inc
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes Yes Yes Yes
Part Number
Yes - 8/20/2009Nomenclature
NSN5034T28P01
CSI /
Date
No. 6 Annular Ball Bearing
3110-01-097-2292
M D I Critical Characteristic
Y N N Outer Ring OD.
Y N N MPI Limits (allowable indications) per P29TF39 CL-A, Para. 3.2.2.4.3 , Table 4.
Y N N Nital Etch, overheating per M50TF5 CL-A, Para 4.1.6.1.
Y N N Hardness per Engineering Requirements and C50TF56 CL-A, Para. 3.3.1.
Y N N Inner Ring ID.
Y N N Max Permissible Surface E conditions per P29TF39 CL-A, Para. 3.2.2.4.1.1 (b) , Table 2.
Y N N Radial Internal Clearance, IRC.
N Y N Radial Internal Clearance.
N Y N Outside Diameter.
N Y N Bore Diameter.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Page 3 of 15M&O Critical Safety Items - T359
Yes - 11/3/2005Nomenclature
NSN5043T75G33
CSI /
Date
Power Turbine Rotor Assy
6105-01-673-5316
M D I Critical Characteristic
Y Y N This assembly contains Critical Safety item parts per P1TF94.
Y N N Perform 10X visual inspection on material removal locations 2 and 5 per Drawing 5043T75, Note 15. No cracks allowed.
N Y N White Light Inspect Verification of an absence of cracks after balance grind on Stage 3 and Stage 4 turbine disks.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes No Yes No
Part Number
Yes - 9/15/2023Nomenclature
NSN5060T08P01
CSI /
Date
Stg 3 Disk Forging
M D I Critical Characteristic
Y N N Ultrasonic Inspection per Drawing 5060T08, per Note 4.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes No No No No
Part Number
Yes - 9/15/2023Nomenclature
NSN5060T09P01
CSI /
Date
Stg 4 Disk Forging
M D I Critical Characteristic
Y N N Ultrasonic Inspection per Drawing 5060T09, Note 4.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes No No No No
Part Number NSN5121T23P02
Page 4 of 15M&O Critical Safety Items - T359
Yes - 11/17/2022Nomenclature CSI / Date
Power Turbine Shaft Forging
M D I Critical Characteristic
Y N N Billet Shall conform to Spec. P1TF77, Para 3.6.2 per Drawing 5121T23, Note 12H.
Y N N Billet Shall conform to Spec. P1TF77, Para. 3.6.2 per Drawing 5121T23, Note 5.G.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes No No No No
Part Number
Yes - 11/17/2022Nomenclature
NSN5121T23P03
CSI /
Date
Power Turbine Shaft Forging
M D I Critical Characteristic
Y N N Billet Shall conform to Spec. P1TF77, Para 3.6.2 per Drawing 5121T23, Note 5.G.
Y N N Billet Shall conform to Spec. P1TF77, Para. 3.6.2 per Drawing 5121T23, Note 12.H.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes No No No No
Part Number
Yes - 7/1/2010Nomenclature
NSN5125T91P01
CSI /
Date
Shaft,Turbine,Aircraft Gas
2840-01-514-1102
M D I Critical Characteristic
Y N N Fillet Root R (Full), .023 min per Drawing 5125T91, Sht. 5, Zone H7.
Y N N FPI per Drawing 5125T91, Note 4.
N Y N FPI Verification that cracks are within DMWR limits.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes Yes Yes Yes
Part Number
Yes - 7/1/2010Nomenclature
NSN5125T91P01RE
CSI /
Date
Shaft,Turbine,Aircraft Gas
Page 5 of 15M&O Critical Safety Items - T359
M D I Critical Characteristic
N Y N FPI verification that cracks are within DMWR limits
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes Yes Yes Yes
Part Number
Yes - 8/13/2001Nomenclature
NSN5125T92G01
CSI /
Date
Shaft Assy, Power Turbine
2840-01-473-3556
M D I Critical Characteristic
Y Y N This assembly contains Critical Safety item parts per P1TF94.
N Y N 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.
N Y N White Light Inspection Verification of an absence of cracks after balance grind.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes Yes Yes Yes
Part Number
Yes - 11/2/2005Nomenclature
NSN6038T32P01
CSI /
Date
Disc, Turbine, Stage 3
2840-01-082-8365
M D I Critical Characteristic
Y N N Non-conventional machining material removal, no recast layer allowed, no intergranular attack allowed, no cracks allowed, per note 6 of drawing
Y N N Hardness on raw material forging drwg (see zone A4 of drwg for forging)
Y N N Results of ultrasonic inspection of forging (see zone A4 of drwg for forging)
Y N N Absence of cracks via fluorescent penetrant inspection per drawing note 3
N Y N Absence of cracks via White Light Inspection per DMWR requirements; following a balance grind operation
N Y N Absence of cracks via FPI per DMWR requirements; except following a balance grind operation
N Y N Diameter E per DMWR Limits
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes No Yes No
Page 6 of 15M&O Critical Safety Items - T359
Yes - 3/30/2005Nomenclature
NSN6038T32P02
CSI /
Date
Disc, Turbine, Stage 3
2840-01-517-5432
M D I Critical Characteristic
Y N N Make from forging P/N 5060T08P01.
Y N N Fluorescent penetrant inspection (FPI) per Drawing 6038T32, Note 3.
N Y N White Light Inspection Verification of an absence of cracks after balance grind.
N Y N FPI Verification of absence of cracks except following a balance grind operation.
N Y N Diameter E.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes No Yes No
Part Number
Yes - 11/2/2005Nomenclature
NSN6038T34P05
CSI /
Date
Disc, Turbine, Stage 4
2840-01-287-9668
M D I Critical Characteristic
Y N N Shot peening per note 26 of drwg
Y N N Ultrasonic Inspection of forgings per note 21
Y N N Hardness
Y Y N Diameter "H"
Y N N Contour limits of dovetail slots are to be met on all surfaces on both sides of slot simultaneously
Y N N Fluorescent penetrant inspection
N Y N Absence of cracks via White Light Inspection per DMWR requirements; following a balance grind operation
N Y N Absence of cracks via FPI per DMWR requirements; except following a balance grind operation
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes No Yes No
Part Number
Yes - 3/30/2005Nomenclature
NSN6038T34P06
CSI /
Date
Disc, Turbine, Stage 4
2840-01-517-5429
M D I Critical Characteristic
Y N N Make from forging P/N 5060T09P01.
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Page 7 of 15M&O Critical Safety Items - T359
Y N N Fluorescent penetrant inspection (FPI) per Drawing 6038T34, Note 3.
N Y N White Light Inspection Verification of an absence of cracks after balance grind.
N Y N FPI Verification of absence of cracks except following a balance grind operation.
N Y N Diameter H.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Part Number
Yes - 11/3/2005Nomenclature
NSN6038T39P09
CSI /
Date
Stage 3 Turbine Blade
2840-01-493-9821
M D I Critical Characteristic
Y N N FPI per Drawing 6038T39, per Note 20 and Zone H10, Note 1.4, No linear indications allowed.
Y N N FPI per Drawing 6038T39, per Note 20 and Zone J10, Note 1.2, Minimum space between indications.
N Y N FPI Verification or White Light Inspection Verification of an absence of cracks as applicable.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes No Yes No
Part Number
Yes - 9/15/2023Nomenclature
NSN6038T40P02
CSI /
Date
Stage 4 Turbine Blade Casting
M D I Critical Characteristic
Y N N Radiological Inspect per Drawing 6038T40, Note 17 and P3TF5 CL-A.
Y N N Per drawing 6038T40, zone J14, fluorescent penetrant & visual inspection table, 1.5 no linear indications allowed.
Y N N Per drawing 6038T40, zone J14, fluorescent penetrant & visual inspection table, 1.2 minimum spacing for negative indications.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
No Yes Yes Yes No
Part Number
Yes - 2/1/1994Nomenclature
NSN6038T41P02
CSI /
Date
Blade, Turbine
2840-01-087-4291
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Page 8 of 15M&O Critical Safety Items - T359
Y N N Indications appearing directly opposite and apparently going through the casting are not acceptable,” per drawing 6038T41, note 16e.
N Y N FPI Verification or White Light Inspection Verification of an absence of cracks as applicable.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Part Number
Yes - 7/1/2010Nomenclature
NSN6043T34P01
CSI /
Date
Shaft,Turbine,Aircraft Gas
2840-01-514-1102
M D I Critical Characteristic
Y N N FPI per Drawing 6043T34 note 4
N Y N FPI verification that cracks are within DMWR limits.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes Yes Yes Yes
Part Number
Yes - 8/26/2015Nomenclature
NSN6064T36P01
CSI /
Date
#6 Annular Ball, Separable
3110-01-097-2292
M D I Critical Characteristic
Y N N Outer Ring OD 3.3462 - 3.3465 in. per Drawing 6064T36, Zone B12.
Y N N Max Permissible Surface conditions per P29TF39 CL-A, Para. 3.2.2.4.1.1 (b), Table II.
Y N N Radial Internal Clearance .0039 - .0047 in. per Drawing 6064T36, Zone H12, Engineering Requirement #2.
Y N N MPI Limits (allowable indications) per P29TF39 CL-A, Para. 3.2.2.4.3, Table IV.
Y N N Nital etch inspection per M50TF32 CL-A, Para. 4.1.6.1 Overheating.
Y N N Hardness Rockwell C 60 to 64 per Drawing 6064T36, Zone F12, Engineering Requirement #13.
Y N N Bore Diameter 1 .5746 - 1.5748 in. per Drawing 6064T36, Zone B11.
N Y N Radial Internal Clearance per Engine DMWR.
N Y N Outside Diameter per Engine DMWR.
N Y N Bore Diameter per Engine DMWR.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
78118 Timken Aerospace
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Page 9 of 15M&O Critical Safety Items - T359
Yes - 10/28/2013Nomenclature
NSN6064T36P02
CSI /
Date
#6 Annular Ball, Separable
3110-01-097-2292
M D I Critical Characteristic
Y N N Outer Ring OD 3.3462 - 3.3465 in. per Drawing 6064T36, Zone B12.
Y N N Max Permissible Surface conditions per P29TF39 CL-A, Para. 3.2.2.4.1.1 (b), Table II.
Y N N Radial Internal Clearance .0039 - .0047 in. per Drawing 6064T36, Zone H12, Engineering Requirement #2.
Y N N MPI Limits (allowable indications) per P29TF39 CL-A, Para. 3.2.2.4.3, Table IV.
Y N N Nital etch inspection per M50TF32 CL-A, Para. 4.1.6.1 Overheating.
Y N N Hardness Rockwell C 60 to 64 per Drawing 6064T36, Zone F12, Engineering Requirement #13.
Y N N Bore Diameter 1 .5746 - 1.5748 in. per Drawing 6064T36, Zone B11.
N Y N Radial Internal Clearance per Engine DMWR.
N Y N Outside Diameter per Engine DMWR.
N Y N Bore Diameter per Engine DMWR.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
36069 Schaeffler Aerospace Canada Inc
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes Yes Yes Yes
Part Number
Yes - 8/27/2010Nomenclature
NSN6064T37P01
CSI /
Date
No. 6 Annular Ball
3110-01-097-2292
M D I Critical Characteristic
Y N N Outer Ring OD 3.3462 - 3.3465 in. per Drawing 6064T37, Zone B12.
Y N N Max Permissible Surface conditions per P29TF39 CL-A, Para. 3.2.2.4.1.1 (b), Table II.
Y N N Radial Internal Clearance .0039 - .0047 in. per Drawing 6064T37, Zone H12, Engineering Requirement #2.
Y N N MPI Limits (allowable indications) per P29TF39 CL-A, Para. 3.2.2.4.3, Table IV.
Y N N Nital etch inspection per M50TF32 CL-A; Para. 4.1.6.1 Overheating.
Y N N Hardness Rockwell C 60 to 64 per Drawing 6064T37, Zone F12, Engineering Requirement #13.
Y N N Bore Diameter 1 .5746 - 1.5748 in. per Drawing 6064T37, Zone B11.
N Y N Radial Internal Clearance per Engine DMWR.
N Y N Outside Diameter per Engine DMWR.
N Y N Bore Diameter per Engine DMWR.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
38443 SKF USA Inc
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes Yes Yes Yes
Part Number NSN6064T80P01 3110-01-084-2368
Page 10 of 15M&O Critical Safety Items - T359
Yes - 8/20/2009Nomenclature CSI / Date
# 5 Bearing, Roller
M D I Critical Characteristic
Y N N Outer Ring OD 2.6769 - 2.6772 in. per Drawing 6064T80, Zone C9.
Y N N Max Permissible Surface Conditions per P29TF39 CL-A, Para. 3.2.2.4.1.1 (b), Table II.
Y N N MPI Limits (allowable indications) per P29TF39 CL-A, Para. 3.2.2.4.3, Table IV.
Y N N Nital Etch per M50TF32 CL-A, Para 4.1.6.1, Overheating.
Y N N Radial Internal Clearance .0010 - .0014 in. per Drawing 6064T80, Zone H12, Engineering Requirement #2.
Y N N Hardness Rockwell C 60 - 64 per Drawing 6064T80, Zone F12, Engineering Requirement #12.
Y N N Inner Ring Bore Diameter 1.5766 - 1.5768 in. per Drawing 6064T80, Zone B10.
N Y N Radial Internal Clearance per Engine DMWR.
N Y N Outside Diameter per Engine DMWR.
N Y N Bore Diameter per Engine DMWR.
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
38443 SKF USA Inc
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes Yes Yes Yes
Part Number
NoNomenclature
NSN4903T21P01
CSI /
Date
Bushing, Flanged (procure for O/H only)
3120-01-346-9151
M D I Critical Characteristic
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
No Yes Yes Yes Yes
Part Number
NoNomenclature
NSN6039T12P01
CSI /
Date
Bearing, Support
3130-01-089-4120
M D I Critical Characteristic
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
No Yes No Yes No
Page 11 of 15M&O Critical Safety Items - T359
NoNomenclature
NSN6038T37G01
CSI /
Date
Seal & Nozzle Assy
2840-01-087-4299
M D I Critical Characteristic
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes No Yes No
Part Number
NoNomenclature
NSN6055T07G01
CSI /
Date
Seal, Stationary, Air
2840-01-247-9514
M D I Critical Characteristic
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes No Yes No
Part Number
NoNomenclature
NSN5901T09P02
CSI /
Date
Seal, Air, Aircraft Gas Turbine Engine
2840-01-353-4539
M D I Critical Characteristic
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
No Yes Yes No No
Part Number
NoNomenclature
NSN6038T37G02
CSI /
Date
Seal & Nozzle Assy
2840-01-242-1758
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Page 12 of 15M&O Critical Safety Items - T359
99207 General Electric Company (Aircraft Engine Business Group)
Part Number
NoNomenclature
NSN4903T21P02
CSI /
Date
Bushing, Flanged (procure for O/H only)
3120-01-347-0637
M D I Critical Characteristic
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
No Yes Yes Yes Yes
Part Number
NoNomenclature
NSN6058T13G11
CSI /
Date
Nozzle Duct & Air Seal Assy
2840-01-362-4935
M D I Critical Characteristic
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes No Yes No
Part Number
NoNomenclature
NSN6039T12P02
CSI /
Date
Bearing, Support
3130-01-221-6025
M D I Critical Characteristic
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
2V343 Apex Manufacturing Company Inc
06320 Aerocision LLC
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Page 13 of 15M&O Critical Safety Items - T359
NoNomenclature
NSN4903T20P01
CSI /
Date
Bushing, Flanged (procure for O/H only)
3120-01-346-3551
M D I Critical Characteristic
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
03350 General Electric Supply Company (Support Services Opns)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
No Yes Yes Yes Yes
Part Number
NoNomenclature
NSN5056T27G02
CSI /
Date
Seal, Air
2840-01-249-1072
M D I Critical Characteristic
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
50554 Metro Machine Works Inc
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Yes Yes Yes Yes Yes
Part Number
NoNomenclature
NSN5901T09P01
CSI /
Date
Seal, Honeycomb (procure for O/H only)
2840-01-353-4540
M D I Critical Characteristic
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
No Yes Yes Yes Yes
Part Number
NoNomenclature
NSN6038T37G07
CSI /
Date
Seal & Nozzle Assy
2840-01-419-2224
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Page 14 of 15M&O Critical Safety Items - T359
99207 General Electric Company (Aircraft Engine Business Group)
Part Number
NoNomenclature
NSN5088T39G04
CSI /
Date
Shroud Segment Assy, Turbine
2840-01-425-5361
M D I Critical Characteristic
CAGE Approved Replacement (M&O) Source Name
99207 General Electric Company (Aircraft Engine Business Group)
Serial Number Req'd Engineering Test Req'd Fatigue Endurance Interchange
Page 15 of 15M&O Critical Safety Items - T359
File details come from the government source that posted it. Updated .