530082: HUB,COMPRESSOR,AIRCRAFT GAS TURB.
HUB,COMPRESSOR,AIRCRAFT GAS TURB. Key specifications include diameter: 18.740 INCHES MINIMUM AND 18.760 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 16.500 INCHES MINIMUM AND 16.570 INCHES MAXIMUM IN, special_features: ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE, end_item_identification: ENGINE MODEL TF33, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2010-00-727-1886, 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 | 18.740 INCHES MINIMUM AND 18.760 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| overall_length | 16.500 INCHES MINIMUM AND 16.570 INCHES MAXIMUM IN |
| special_features | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| end_item_identification | ENGINE MODEL TF33 |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS 5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2010-00-727-1886 |
| PROPELLER TYPE | FIXED PITCH |
| DESIGN PITCH | 3.500 FEET FT |
| SPAN MAXIMUM DIAMETER | 4.000 FEET FT |
| ROTATION DIRECTION | RIGHT-HAND |
| BLADE QUANTITY | 4 |
| BLADE PITCH TYPE | CONSTANT |
| MATERIAL | COPPER ALLOY OVERALL |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY PAC AMWW |