739201: DISK AND HUB,COMPRESSOR,AIRCRAFT.
DISK AND HUB,COMPRESSOR,AIRCRAFT. Key specifications include design_type: AXIAL COMPRESSOR, end_item_identification: TF33-PW-102/A&B/103 AIRCRAFT GAS TURBINE ENGINES, engine_section_location: COMPRESSOR, reference_data_and_literature: T.O. 2J-TF33-34, FIG 5, IND 1, criticality_code_justification: FEAT, part_name_assigned_by_controlling_agency: ORIGINAL NAME HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-450-9428, 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 |
| end_item_identification | TF33-PW-102/A&B/103 AIRCRAFT GAS TURBINE ENGINES |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O. 2J-TF33-34, FIG 5, IND 1 |
| criticality_code_justification | FEAT |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-450-9428 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 5, IND 1 |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | USED ON THE ROTOR FRONT COMPRESSOR; SUPERSEDES P/N 431001; THE CRITICALITY CODE CHANGE TO F IS ESSENTIAL TO WEAPON SYSTEM PERFORMANCE AND OPERATION. A FAILURE COULD CAUSE CATASTROPHIC FAILURE RESULTING IN THE LOSS OF OR SERIOUS DAMAGE TO THE AIRCRAFT OR WEAPON SYSTEM OR AN UNCOMMANDED ENGINE SHUTDOWN THAT JEPORDIZES SAFETY |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF33-PW-102/A&B/103 AIRCRAFT GAS TURBINE ENGINES |
No substitute or cross-reference records for this part.