7055M94P01: DISK AND HUB,COMPRESSOR,AIRCRAFT.
DISK AND HUB,COMPRESSOR,AIRCRAFT. Key specifications include diameter: 18.845 INCHES MINIMUM AND 18.855 INCHES MAXIMUM IN, material: STEEL DISK, design_type: AXIAL COMPRESSOR, overall_length: 5.818 INCHES MINIMUM AND 5.860 INCHES MAXIMUM IN, special_features: WAS DISK AND HUB,AXIAL COMPRESSOR,TURBINE ENGINE, end_item_identification: J79 ENG. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-071-8398, 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 | 18.845 INCHES MINIMUM AND 18.855 INCHES MAXIMUM IN |
| material | STEEL DISK |
| design_type | AXIAL COMPRESSOR |
| overall_length | 5.818 INCHES MINIMUM AND 5.860 INCHES MAXIMUM IN |
| special_features | WAS DISK AND HUB,AXIAL COMPRESSOR,TURBINE ENGINE |
| end_item_identification | J79 ENG |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-071-8398 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 18.845 INCHES MINIMUM AND 18.855 INCHES MAXIMUM IN |
| OVERALL LENGTH | 5.818 INCHES MINIMUM AND 5.860 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | WAS DISK AND HUB,AXIAL COMPRESSOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | J79 ENG |
| MATERIAL | STEEL DISK |
| MATERIAL | STEEL HUB |
No substitute or cross-reference records for this part.