7-4643-1: DISK AND HUB,COMPRESSOR,AIRCRAFT.
DISK AND HUB,COMPRESSOR,AIRCRAFT. Key specifications include diameter: 5.1183 INCHES MINIMUM AND 5.1189 INCHES MAXIMUM IN, design_type: AXIAL COMPRESSOR, special_features: USED ON THE ROTOR FRONT COMPRESSOR, end_item_identification: TF33PW-3/5/9/102/A&B AIRCRAFT GAS TURBINE ENGINES, engine_section_location: COMPRESSOR, reference_data_and_literature: T.O. 2J-TF33-34, FIG 5, IND 4.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-161-1130, 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 | 5.1183 INCHES MINIMUM AND 5.1189 INCHES MAXIMUM IN |
| design_type | AXIAL COMPRESSOR |
| special_features | USED ON THE ROTOR FRONT COMPRESSOR |
| end_item_identification | TF33PW-3/5/9/102/A&B AIRCRAFT GAS TURBINE ENGINES |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O. 2J-TF33-34, FIG 5, IND 4 |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-161-1130 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 5, IND 4 |
| DIAMETER | 5.1183 INCHES MINIMUM AND 5.1189 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | USED ON THE ROTOR FRONT COMPRESSOR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF33PW-3/5/9/102/A&B AIRCRAFT GAS TURBINE ENGINES |
No substitute or cross-reference records for this part.