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 product is currently in active production with full OEM support.
This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 5998-01-091-2394, 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 | 5998-01-091-2394 |
| FEATURES PROVIDED | ELECTROSTATIC SENSITIVE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | MUX INTERFACE |
| SPECIAL FEATURES | CAP 64; CRYSTAL 1, DIODE 16, MCKT 32, PWB 1, RES 37, SOLENOID 2, TRANSISTOR 2 |
| CRITICALITY CODE JUSTIFICATION | CBBL |
| END ITEM IDENTIFICATION | A10 ACFT |
| FEATURES PROVIDED | ELECTROSTATIC SENSITIVE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | MUX INTERFACE |
| SPECIAL FEATURES | CAP 64; CRYSTAL 1, DIODE 16, MCKT 32, PWB 1, RES 37, SOLENOID 2, TRANSISTOR 2 |
| CRITICALITY CODE JUSTIFICATION | CBBL |
| END ITEM IDENTIFICATION | A10 ACFT |