1863M32P01-118: SHAFT,TURBINE,AIRCRAFT GAS TURBI.
SHAFT,TURBINE,AIRCRAFT GAS TURBI. Key specifications include diameter: 10.500 INCHES NOMINAL IN, material: NICKEL ALLOY SHAFT, overall_length: 15.000 INCHES NOMINAL IN, special_features: SURFACE TREATMENT SHOT PEEN, end_item_identification: 2J-F118-4 FIG49 IND 4, engine_section_location: HIGH PRESSURE TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-487-1566, 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 | 10.500 INCHES NOMINAL IN |
| material | NICKEL ALLOY SHAFT |
| overall_length | 15.000 INCHES NOMINAL IN |
| special_features | SURFACE TREATMENT SHOT PEEN |
| end_item_identification | 2J-F118-4 FIG49 IND 4 |
| engine_section_location | HIGH PRESSURE TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-01-487-1566 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 10.500 INCHES NOMINAL IN |
| OVERALL LENGTH | 15.000 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | SURFACE TREATMENT SHOT PEEN |
| END ITEM IDENTIFICATION | 2J-F118-4 FIG49 IND 4 |
| MATERIAL | NICKEL ALLOY SHAFT |
No substitute or cross-reference records for this part.