Part Details | TURBO-SHAFT AIRCRAFT ENGINE
2840-01-533-0397 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: T58GE402, T58-GE-402, 2840-01-533-0397, 01-533-0397, 2840015330397, 015330397
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 29, 2005 | 01-533-0397 | 32600 ( ENGINE, AIRCRAFT, TURBO-SHAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-533-0397
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| T58-GE-402 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-533-0397
| Characteristic | Specifications |
|---|---|
| HORSEPOWER RATING | 1500.0 |
| INCLOSURE | NOT INCLUDED |
| SPECIAL FEATURES | 10 COMPRESSOR STAGES |