9524M58: HUB,TURBINE,AIRCRAFT GAS TURBINE.
HUB,TURBINE,AIRCRAFT GAS TURBINE. Key specifications include diameter: 13.430 INCHES MINIMUM AND 13.441 INCHES MAXIMUM IN, design_type: AXIAL COMPRESSOR, end_item_identification: ACFT ENG F101-GE-100 AND F110-GE-100, engine_section_location: TURBINE, reference_data_and_literature: T.O. 2J-F101-4, FIG 56, IND 22, 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 2840-01-146-9475, 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 | 13.430 INCHES MINIMUM AND 13.441 INCHES MAXIMUM IN |
| design_type | AXIAL COMPRESSOR |
| end_item_identification | ACFT ENG F101-GE-100 AND F110-GE-100 |
| engine_section_location | TURBINE |
| reference_data_and_literature | T.O. 2J-F101-4, FIG 56, IND 22 |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-146-9475 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F101-4, FIG 56, IND 22 |
| DIAMETER | 13.430 INCHES MINIMUM AND 13.441 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F101-GE-100 AND F110-GE-100 |