Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE HUB
2840-01-379-8841 A component of a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to attach to the front and/or rear of the rotor providing support, alignment, and a means of attachment for a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have provisions for installing bearings, and/or oil and air seals. See also DISK AND HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 2189801, 2189801, 2840-01-379-8841, 01-379-8841, 2840013798841, 013798841
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 10, 1993 | 01-379-8841 | 50577 ( HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-379-8841
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2189801 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 2189801 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-379-8841
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | MFR DESCRIBES AS HUB, FRONT COMPRESSOR, FRONT |
| END ITEM IDENTIFICATION | J-52 ENGINE |