851641: DISK AND HUB,COMPRESSOR,AIRCRAFT.
DISK AND HUB,COMPRESSOR,AIRCRAFT. Key specifications include diameter: 15.000 INCHES NOMINAL IN, material: TITANIUM ALLOY HUB, design_type: AXIAL COMPRESSOR, overall_height: 6.500 INCHES NOMINAL IN, special_features: USED ON THE ROTOR FRONT COMPRESSOR, end_item_identification: TF33-PW-102/A & B AIRCRAFT GAS TURBINE-FAN ENGINES. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-362-7057, 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 | 15.000 INCHES NOMINAL IN |
| material | TITANIUM ALLOY HUB |
| design_type | AXIAL COMPRESSOR |
| stage_number | 1 |
| overall_height | 6.500 INCHES NOMINAL IN |
| special_features | USED ON THE ROTOR FRONT COMPRESSOR |
| end_item_identification | TF33-PW-102/A & B AIRCRAFT GAS TURBINE-FAN ENGINES |
| engine_section_location | LOW PRESSURE COMPRESSOR |
| reference_data_and_literature | T.O. 2J-TF33-34, FIG 5, IND 1 |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-362-7057 |
| OVERALL HEIGHT | 6.500 INCHES NOMINAL IN |
| STAGE NUMBER | 1 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 5, IND 1 |
| DIAMETER | 15.000 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | LOW PRESSURE 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 | TF33-PW-102/A & B AIRCRAFT GAS TURBINE-FAN ENGINES |
| MATERIAL | TITANIUM ALLOY HUB |
No substitute or cross-reference records for this part.