9138M62G12 — FRAME,TURBINE,AIRCRAFT GAS TURBI

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9138M62G12: FRAME,TURBINE,AIRCRAFT GAS TURBI.

FRAME,TURBINE,AIRCRAFT GAS TURBI. Key specifications include material: NICKEL ALLOY, overall_length: 13.165 INCHES MINIMUM AND 13.205 INCHES MAXIMUM IN, outside_diameter: 16.160 INCHES MINIMUM AND 16.200 INCHES MAXIMUM IN, end_item_identification: TF-39 AIRCRAFT GAS TURBINE ENGINE, reference_data_and_literature: T.O. 2J-TF39-4, FIG 63, IND 1, criticality_code_justification: ABHP AND ABKV AND FEAT.

This part is cataloged in the U.S. Government catalog under NSN 2840-01-445-0387, indicating validated use in U.S. government and defense logistics supply chains.

Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels. Verify compatibility with your specific system configuration before ordering.

WHERE IT FITS

9138M62G12

NSN: 2840-01-445-0387
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

material	NICKEL ALLOY
overall_length	13.165 INCHES MINIMUM AND 13.205 INCHES MAXIMUM IN
outside_diameter	16.160 INCHES MINIMUM AND 16.200 INCHES MAXIMUM IN
special_features	DCN 97-4, CID 407635; ITEM INTRODUCES A NEW TURBINE MID FRAME ASSEMBLY INCORPORATING A TBC MID FRAME AND WASPALOY BOLTS; REPLACES P/N 9138M62G10
end_item_identification	TF-39 AIRCRAFT GAS TURBINE ENGINE
reference_data_and_literature	T.O. 2J-TF39-4, FIG 63, IND 1
criticality_code_justification	ABHP AND ABKV AND FEAT
NSN	2840-01-445-0387

COMPONENT DIAGRAM

KEY FEATURES

•

CRITICALITY CODE JUSTIFICATION: ABHP AND ABKV AND FEAT

•

REFERENCE DATA AND LITERATURE: T.O. 2J-TF39-4, FIG 63, IND 1

•

OUTSIDE DIAMETER: 16.160 INCHES MINIMUM AND 16.200 INCHES MAXIMUM IN

•

MATERIAL: NICKEL ALLOY

TECHNICAL CHARACTERISTICS

CRITICALITY CODE JUSTIFICATION	ABHP AND ABKV AND FEAT
REFERENCE DATA AND LITERATURE	T.O. 2J-TF39-4, FIG 63, IND 1
OVERALL LENGTH	13.165 INCHES MINIMUM AND 13.205 INCHES MAXIMUM IN
OUTSIDE DIAMETER	16.160 INCHES MINIMUM AND 16.200 INCHES MAXIMUM IN
SPECIAL FEATURES	DCN 97-4, CID 407635; ITEM INTRODUCES A NEW TURBINE MID FRAME ASSEMBLY INCORPORATING A TBC MID FRAME AND WASPALOY BOLTS; REPLACES P/N 9138M62G10
END ITEM IDENTIFICATION	TF-39 AIRCRAFT GAS TURBINE ENGINE
MATERIAL	NICKEL ALLOY

OTHER ITEMS IN FSC 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.

2840-00-004-4242 2840-00-021-4702 2840-00-043-0981 2840-00-043-0982 2840-00-048-5261 2840-00-407-9165 2840-01-171-0875

SUBSTITUTES & CROSS-REFERENCES 1

9138M62Reference document

Same NSN cross-reference

Reference document — Drawing number reference only

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 9138M62G12?

9138M62G12 is a FRAME,TURBINE,AIRCRAFT GAS TURBI.

What parts can replace 9138M62G12?

There is 1 known substitute for 9138M62G12: 9138M62. Substitute compatibility should be verified for your specific system.

What is the NSN for 9138M62G12?

9138M62G12 is cataloged in the U.S. Government catalog under NSN 2840-01-445-0387. This indicates validated use in U.S. government and defense supply chains.

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9138M62G12 — FRAME,TURBINE,AIRCRAFT GAS TURBI

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