Part Details | TURBO-SHAFT AIRCRAFT ENGINE
2840-01-353-7635 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: 200102032, 2-001-020-32, T55L714, T-55-L-714, 2840-01-353-7635, 01-353-7635, 2840013537635, 013537635
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 15, 1992 | 01-353-7635 | 32600 ( ENGINE, AIRCRAFT, TURBO-SHAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-353-7635
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2-001-020-32 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| T-55-L-714 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-353-7635
| Characteristic | Specifications |
|---|