2182060: SHAFT,TURBINE,AIRCRAFT GAS TURBI.
SHAFT,TURBINE,AIRCRAFT GAS TURBI. Key specifications include material: NICKEL ALLOY OVERALL, special_features: CONIZANT SERVICE:NAVY, end_item_identification: TURBO PROP ENGINE TF30P, material_document_and_classification: PWA 1003, CAGE 77445 MFR REF SINGLE MATERIAL RESPONSE OVERALL. This part is cataloged in the U.S.
Government catalog under NSN 2990-00-734-2371, 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.
| material | NICKEL ALLOY OVERALL |
| special_features | CONIZANT SERVICE:NAVY |
| end_item_identification | TURBO PROP ENGINE TF30P |
| material_document_and_classification | PWA 1003, CAGE 77445 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2990-00-734-2371 |
| OPERATING POSITION | HORIZONTAL |
| INLET OUTSIDE DIAMETER | 2.625 INCHES NOMINAL SINGLE INLET IN |
| INLET LOCATION | CENTRALLY LOCATED IN END SECTION OF BODY |
| COOLANT TYPE | AIR |
| DESIGN TYPE | DRY |
| OVERALL DIAMETER | 5.875 INCHES MINIMUM AND 6.125 INCHES MAXIMUM IN |
| OUTLET INSIDE DIAMETER | 2.005 INCHES MINIMUM AND 2.010 INCHES MAXIMUM FIRST OUTLET IN |
| INLET PROJECTION LENGTH | 1.250 INCHES NOMINAL SINGLE INLET IN |
| BAFFLE QUANTITY | 1 |
| OVERALL LENGTH | 21.875 INCHES MINIMUM AND 22.125 INCHES MAXIMUM IN |