9138M62: 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.
| 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 |
| 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 |
No substitute or cross-reference records for this part.