9945M27G01: HUB,TURBINE,AIRCRAFT GAS TURBINE.
HUB,TURBINE,AIRCRAFT GAS TURBINE. Key specifications include diameter: 14.980 INCHES MINIMUM AND 15.000 INCHES MAXIMUM IN, material: STEEL OVERALL, overall_length: 6.280 INCHES MINIMUM AND 6.320 INCHES MAXIMUM IN, special_features: ORIGINAL NAME HUB,TURBINE,TURBINE ENGINE, end_item_identification: ACFT ENG F101, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-174-5736, 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 | 14.980 INCHES MINIMUM AND 15.000 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| overall_length | 6.280 INCHES MINIMUM AND 6.320 INCHES MAXIMUM IN |
| special_features | ORIGINAL NAME HUB,TURBINE,TURBINE ENGINE |
| end_item_identification | ACFT ENG F101 |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS 5798 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-174-5736 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5798 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 14.980 INCHES MINIMUM AND 15.000 INCHES MAXIMUM IN |
| OVERALL LENGTH | 6.280 INCHES MINIMUM AND 6.320 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | ORIGINAL NAME HUB,TURBINE,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F101 |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.