4051523: HUB,COMPRESSOR,AIRCRAFT GAS TURB.
HUB,COMPRESSOR,AIRCRAFT GAS TURB. Key specifications include diameter: 4.780 INCHES MINIMUM AND 4.800 INCHES MAXIMUM IN, material: TITANIUM ALLOY OVERALL, overall_length: 1.920 INCHES MINIMUM AND 1.940 INCHES MAXIMUM IN, special_features: ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE, end_item_identification: ACFT ENG F100, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-107-8270, 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 | 4.780 INCHES MINIMUM AND 4.800 INCHES MAXIMUM IN |
| material | TITANIUM ALLOY OVERALL |
| overall_length | 1.920 INCHES MINIMUM AND 1.940 INCHES MAXIMUM IN |
| special_features | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| end_item_identification | ACFT ENG F100 |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-107-8270 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 4.780 INCHES MINIMUM AND 4.800 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.920 INCHES MINIMUM AND 1.940 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F100 |
| MATERIAL | TITANIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.