1275M25P02-110: 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; SIMILAR TO 1359M21P02 USED ON THE F110-GE-100 BUT FOR THE F110-GE-110 ENGINE ONLY, end_item_identification: F110-GE-110 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: LOW PRESSURE TURBINE, criticality_code_justification: FEAT, part_name_assigned_by_controlling_agency: ORIGINAL NAME SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-447-4158, 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; SIMILAR TO 1359M21P02 USED ON THE F110-GE-100 BUT FOR THE F110-GE-110 ENGINE ONLY |
| end_item_identification | F110-GE-110 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | LOW PRESSURE TURBINE |
| criticality_code_justification | FEAT |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-447-4158 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| SPECIAL FEATURES | T.O. 2J-F110-4, FIG 58, IND 38; SIMILAR TO 1359M21P02 USED ON THE F110-GE-100 BUT FOR THE F110-GE-110 ENGINE ONLY |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | F110-GE-110 AIRCRAFT GAS TURBINE ENGINE |