Part Details | TURBO-SHAFT AIRCRAFT ENGINE
2840-00-621-1860 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: 100006023, 1-000-060-23, T53L703, T53-L-703, 2840-00-621-1860, 00-621-1860, 2840006211860, 006211860
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 27, 1975 | 00-621-1860 | 32600 ( ENGINE, AIRCRAFT, TURBO-SHAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-621-1860
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-000-060-23 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| T53-L-703 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-00-621-1860
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | AH-1 UH-1 OV-1 TURBINE ENGINE |