753528: 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, overall_length: 12.726 INCHES NOMINAL IN, special_features: ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE, end_item_identification: ACFT ENG TF33, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-160-6504, 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 |
| overall_length | 12.726 INCHES NOMINAL IN |
| special_features | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| end_item_identification | ACFT ENG TF33 |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS 6415 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-160-6504 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6415 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 | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |
| MATERIAL | STEEL OVERALL |