635498: HUB,COMPRESSOR,AIRCRAFT GAS TURB.
HUB,COMPRESSOR,AIRCRAFT GAS TURB. Key specifications include diameter: 16.741 INCHES MINIMUM AND 16.743 INCHES MAXIMUM IN, material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 12.726 INCHES NOMINAL IN, end_item_identification: TF-33 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-458-2759, 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 | 16.741 INCHES MINIMUM AND 16.743 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 12.726 INCHES NOMINAL IN |
| end_item_identification | TF-33 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | T.O. 2J-TF33-34, FIG 6, IND 51 |
| criticality_code_justification | FEAT AND ABHP AND ABMZ AND CZBJ |
| material_document_and_classification | AMS6415 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-458-2759 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT AND ABHP AND ABMZ AND CZBJ |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 6, IND 51 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS6415 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 16.741 INCHES MINIMUM AND 16.743 INCHES MAXIMUM IN |
| OVERALL LENGTH | 12.726 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | P/N NOT TO BE PROCURED; P/N TAKEN OFF ENGINE AND PUT INTO SUPPLY THEN REWORKED UP TO P/N 753538 (01-160-6504); DEPENDING ON REPAIR IT WILL GET ASSIGNED A DIFFERENT P/N; IF THIS P/N HAS CRACKS IN THE TIE ROD HOLES WILL BE ASSIGNED P/N 784473; IF THIS ITEM HAS NOCRACKS, IS REWORKED TO P/N 774659 |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.