746441: DISK AND HUB,COMPRESSOR,AIRCRAFT.
DISK AND HUB,COMPRESSOR,AIRCRAFT. Key specifications include material: TITANIUM ALLOY DISK, design_type: AXIAL COMPRESSOR, overall_height: 6.500 INCHES NOMINAL IN, overall_length: 15.000 INCHES NOMINAL IN, special_features: USED ON THE ROTOR FRONT COMPRESSOR, end_item_identification: TF33-3/5/9/102/A&B/103 AIRCRAFT GAS TURBINE ENGINES. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-442-3548, 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.
| material | TITANIUM ALLOY DISK |
| design_type | AXIAL COMPRESSOR |
| stage_number | 1 |
| overall_height | 6.500 INCHES NOMINAL IN |
| overall_length | 15.000 INCHES NOMINAL IN |
| special_features | USED ON THE ROTOR FRONT COMPRESSOR |
| end_item_identification | TF33-3/5/9/102/A&B/103 AIRCRAFT GAS TURBINE ENGINES |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O. 2J-TF33-4, FIG 5B, IND 1 |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME HUB COMPRESSOR |
| NSN | 2840-01-442-3548 |
| OVERALL HEIGHT | 6.500 INCHES NOMINAL IN |
| STAGE NUMBER | 1 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG 5B, IND 1 |
| OVERALL LENGTH | 15.000 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | USED ON THE ROTOR FRONT COMPRESSOR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME HUB COMPRESSOR |
| END ITEM IDENTIFICATION | TF33-3/5/9/102/A&B/103 AIRCRAFT GAS TURBINE ENGINES |
| MATERIAL | TITANIUM ALLOY DISK |
No substitute or cross-reference records for this part.