HUB,COMPRESSOR,AIRCRAFT GAS TURB. Key specifications include diameter: 18.802 INCHES MINIMUM AND 18.806 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 16.485 INCHES MINIMUM AND 16.505 INCHES MAXIMUM 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 Federal Logistics Information System (FLIS) under NSN 2840-01-160-6505, 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 | 18.802 INCHES MINIMUM AND 18.806 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| overall_length | 16.485 INCHES MINIMUM AND 16.505 INCHES MAXIMUM 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 5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-160-6505 |
| DIAMETER | 18.802 INCHES MINIMUM AND 18.806 INCHES MAXIMUM IN |
| OVERALL LENGTH | 16.485 INCHES MINIMUM AND 16.505 INCHES MAXIMUM IN |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL | NICKEL ALLOY OVERALL |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |
| SPECIAL FEATURES | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| ENGINE SECTION LOCATION | COMPRESSOR |