Part Details | AIRCRAFT GAS TURBINE ENGINE
2840-01-502-5179 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: 1037470109, 2840-01-502-5179, 01-502-5179, 2840015025179, 015025179
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 07, 2002 | 01-502-5179 | 50488 ( ENGINE, GAS TURBINE, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-502-5179
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1037470109 | 24235 | WILLIAMS INTERNATIONAL CO., L.L.C. |
Technical Data | NSN 2840-01-502-5179
| Characteristic | Specifications |
|---|---|
| FUEL TYPE | JET FUEL |
| POWER OUTPUT FOR WHICH DESIGNED | PNEUMATIC/SHAFT |
| MOUNTING TYPE | ANY ACCEPTABLE |
| REFERENCE DATA AND LITERATURE | 2J-F112-4 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F112-WR-100 |