Part Details | AIRCRAFT GAS TURBINE ENGINE
2840-01-562-0110 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: 2216M10G01, 2840-01-562-0110, 01-562-0110, 2840015620110, 015620110
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 26, 2008 | 01-562-0110 | 50488 ( ENGINE, GAS TURBINE, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-562-0110
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2216M10G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-562-0110
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | AUGMENTED TURBOFAN |