9687M80G37: SHAFT,TURBINE,AIRCRAFT GAS TURBI.
SHAFT,TURBINE,AIRCRAFT GAS TURBI. Key specifications include diameter: 23.400 INCHES NOMINAL IN, material: NICKEL ALLOY SHAFT, design_type: AXIAL COMPRESSOR, overall_length: 18.372 INCHES MINIMUM AND 18.390 INCHES MAXIMUM IN, end_item_identification: TF-39 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: HIGH PRESSURE TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-397-4774, 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.
| diameter | 23.400 INCHES NOMINAL IN |
| material | NICKEL ALLOY SHAFT |
| design_type | AXIAL COMPRESSOR |
| overall_length | 18.372 INCHES MINIMUM AND 18.390 INCHES MAXIMUM IN |
| special_features | MATL IS MADE FROM A NEW TRIPLE MELT INCONEL ALLOY; INVOLUTE SPLINE DATA: NO. OF TEETH 65; PITCH 10; PRESSURE ANGLE 14 DEG. 30 MIN. |
| end_item_identification | TF-39 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | HIGH PRESSURE TURBINE |
| criticality_code_justification | ABHP AND CZBJ AND ABMZ AND FEAT |
| NSN | 2840-01-397-4774 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | ABHP AND CZBJ AND ABMZ AND FEAT |
| DIAMETER | 23.400 INCHES NOMINAL IN |
| OVERALL LENGTH | 18.372 INCHES MINIMUM AND 18.390 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | MATL IS MADE FROM A NEW TRIPLE MELT INCONEL ALLOY; INVOLUTE SPLINE DATA: NO. OF TEETH 65; PITCH 10; PRESSURE ANGLE 14 DEG. 30 MIN. |
| END ITEM IDENTIFICATION | TF-39 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY SHAFT |
No substitute or cross-reference records for this part.