1385M21P01-118: SHAFT,TURBINE,AIRCRAFT GAS TURBI.
SHAFT,TURBINE,AIRCRAFT GAS TURBI. Key specifications include design_type: AXIAL COMPRESSOR, special_features: SAME AS CORE P/N 1385M21P01 BUT ONLY TO BE USED ON THE F118 ENGINE, end_item_identification: F118-GE-100 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: HIGH PRESSURE TURBINE, criticality_code_justification: FEAT. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-443-4084, 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.
| design_type | AXIAL COMPRESSOR |
| special_features | SAME AS CORE P/N 1385M21P01 BUT ONLY TO BE USED ON THE F118 ENGINE |
| end_item_identification | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | HIGH PRESSURE TURBINE |
| criticality_code_justification | FEAT |
| NSN | 2840-01-443-4084 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | SAME AS CORE P/N 1385M21P01 BUT ONLY TO BE USED ON THE F118 ENGINE |
| END ITEM IDENTIFICATION | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.