Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE HUB
2840-01-318-4403 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: 2188107, 2188107, 2840-01-318-4403, 01-318-4403, 2840013184403, 013184403
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 19, 1990 | 01-318-4403 | 50577 ( HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-318-4403
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2188107 | 53661 | CAREER SYSTEMS DEVELOPMENT CORP |
| 2188107 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-318-4403
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | 2840-01-314-0707 COMPRESSOR, AXIAL, TURBINE J52-P-6A ENGINE |
| FSC APPLICATION DATA | ROTOR-STATOR COMPRESSOR N2 |