1385M24P05-118: HUB,TURBINE,AIRCRAFT GAS TURBINE.
HUB,TURBINE,AIRCRAFT GAS TURBINE. Key specifications include material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, special_features: SAME AS P/N 1385M24P05 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: CZBJ AND FEAT. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-443-4068, 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 |
| design_type | AXIAL COMPRESSOR |
| special_features | SAME AS P/N 1385M24P05 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 | CZBJ AND FEAT |
| material_document_and_classification | INCONEL 718 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-443-4068 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | CZBJ AND FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | INCONEL 718 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | SAME AS P/N 1385M24P05 BUT ONLY TO BE USED ON THE F118 ENGINE |
| END ITEM IDENTIFICATION | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.