805231: DISK AND HUB,COMPRESSOR,AIRCRAFT.
DISK AND HUB,COMPRESSOR,AIRCRAFT. Key specifications include diameter: 15.000 INCHES NOMINAL IN, material: TITANIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 6.500 INCHES NOMINAL IN, special_features: USED ON THE ROTOR FRONT COMPRESSOR; SUPERSEDED P/N 576901, 395001 AND 747231, end_item_identification: TF33-PW-3/5/9/PW-103 AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-363-0850, 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 OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 6.500 INCHES NOMINAL IN |
| special_features | USED ON THE ROTOR FRONT COMPRESSOR; SUPERSEDED P/N 576901, 395001 AND 747231 |
| end_item_identification | TF33-PW-3/5/9/PW-103 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O. 2J-TF33-4, FIG 5, 5B, IND 1, FIG 5C, IND 6 |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-363-0850 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG 5, 5B, IND 1, FIG 5C, IND 6 |
| DIAMETER | 15.000 INCHES NOMINAL IN |
| OVERALL LENGTH | 6.500 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | USED ON THE ROTOR FRONT COMPRESSOR; SUPERSEDED P/N 576901, 395001 AND 747231 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF33-PW-3/5/9/PW-103 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | TITANIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.