Part Details | TURBO-SHAFT AIRCRAFT ENGINE
2840-01-030-4890 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: 200102023, 2-001-020-23, T55L712, T-55-L-712, 2840-01-030-4890, 01-030-4890, 2840010304890, 010304890
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 07, 1976 | 01-030-4890 | 32600 ( ENGINE, AIRCRAFT, TURBO-SHAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-030-4890
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2-001-020-23 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| T-55-L-712 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-030-4890
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | CH-47 TURBINE ENGINE, ROTARY WING AIRCRAFT |