Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE HUB
2840-00-141-5638 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: 6875431, 6875431, 23089559, 2840-00-141-5638, 00-141-5638, 2840001415638, 001415638
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 12, 1973 | 00-141-5638 | 50577 ( HUB, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-141-5638
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6875431 | 73342 | ALLISON TRANSMISSION, INC. |
| 6875431 | 63005 | ROLLS-ROYCE CORPORATION |
| 23089559 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-00-141-5638
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 9.214 INCHES MINIMUM AND 9.216 INCHES MAXIMUM |
| SPECIAL FEATURES | ORIGINAL NAME HUB,TURBINE,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | T-56 AIRCRAFT ENGINE |