569445: HUB,COMPRESSOR,AIRCRAFT GAS TURB.
HUB,COMPRESSOR,AIRCRAFT GAS TURB. Key specifications include material: TITANIUM ALLOY HUB, design_type: COMPRESSOR, overall_height: 6.415 INCHES NOMINAL IN, overall_length: 18.710 INCHES NOMINAL IN, special_features: ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE, end_item_identification: TF-33 AIRCRAFT ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-243-7739, 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 HUB |
| design_type | COMPRESSOR |
| overall_height | 6.415 INCHES NOMINAL IN |
| overall_length | 18.710 INCHES NOMINAL IN |
| special_features | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| end_item_identification | TF-33 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | 2J-TF33-4 FIG 19 |
| criticality_code_justification | AGAV |
| NSN | 2840-00-243-7739 |
| OVERALL HEIGHT | 6.415 INCHES NOMINAL IN |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-TF33-4 FIG 19 |
| OVERALL LENGTH | 18.710 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| MATERIAL | TITANIUM ALLOY HUB |
No substitute or cross-reference records for this part.