Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB
2840-01-513-2050 A component of a ROTOR, COMPRESSOR, 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, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 500133101, 5001331-01, 2840-01-513-2050, 01-513-2050, 2840015132050, 015132050
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 19, 2003 | 01-513-2050 | 50573 ( HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-513-2050
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5001331-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-513-2050
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | AIRBUS A310 AIRCRAFT ENGINE JT9D-7R4 |