Part Details | TURBO-SHAFT AIRCRAFT ENGINE
2840-01-013-1339 A continuous-combustion type engine, may be with or without container, designed to use superheated air to drive a turbine rotor which is connected to the rotorshaft of a helicopter by way of reduction gears.
Alternate Parts: T63A720, T63-A-720, 6887191, T631720, T63-1-720, 6887191, 2840-01-013-1339, 01-013-1339, 2840010131339, 010131339
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 27, 1975 | 01-013-1339 | 32600 ( ENGINE, AIRCRAFT, TURBO-SHAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-013-1339
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| T63-A-720 | 73342 | ALLISON TRANSMISSION, INC. |
| 6887191 | 73342 | ALLISON TRANSMISSION, INC. |
| T63-1-720 | 63005 | ROLLS-ROYCE CORPORATION |
| 6887191 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-013-1339
| Characteristic | Specifications |
|---|---|
| HORSEPOWER RATING | 370.0 |
| SPECIAL FEATURES | SHAFT HP RATING |