Part Details | AIRCRAFT GAS TURBINE ENGINE
2840-01-356-0987 A continuous combustion type engine. Consists primarily of a COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE, CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE and a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It may have an AFTERBURNER, TURBINE ENGINE and/or a fan section. Air is compressed and heated by a combustible fuel and expanded through the turbine. It is designed to furnish a source of rotary shaft, pneumatic power or thrust power. The pneumatic power is obtained by a bleedoff of the engine compressor. For a complete operating power unit, mounted on a base, see POWER UNIT, GAS TURBINE ENGINE.
Alternate Parts: 7030303001, 70303-03001, 2840-01-356-0987, 01-356-0987, 2840013560987, 013560987
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 28, 1992 | 01-356-0987 | 50488 ( ENGINE, GAS TURBINE, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-356-0987
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 70303-03001 | 81996 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 2840-01-356-0987
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | UH-60 TURBINE ENGINE ROTARY WING AIRCRAFT |