1359M20G01-118: SHAFT,TURBINE,AIRCRAFT GAS TURBI.
SHAFT,TURBINE,AIRCRAFT GAS TURBI. Key specifications include design_type: AXIAL COMPRESSOR, special_features: T.O. 2J-F110-4, FIG 58, IND 38; THIS ITEM IS TO BE USED STRICTLY ON THE F118 ENGINE, end_item_identification: F118-GE-100 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: LOW PRESSURE TURBINE, criticality_code_justification: FEAT AND CZBJ.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-447-8978, 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 | T.O. 2J-F110-4, FIG 58, IND 38; THIS ITEM IS TO BE USED STRICTLY ON THE F118 ENGINE |
| end_item_identification | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | LOW PRESSURE TURBINE |
| criticality_code_justification | FEAT AND CZBJ |
| NSN | 2840-01-447-8978 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| SPECIAL FEATURES | T.O. 2J-F110-4, FIG 58, IND 38; THIS ITEM IS TO BE USED STRICTLY ON THE F118 ENGINE |
| END ITEM IDENTIFICATION | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |