Part Details | AIRCRAFT GAS TURBINE ENGINE
2840-01-629-1592 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: 4135100, 2840-01-629-1592, 01-629-1592, 2840016291592, 016291592
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 19, 2014 | 01-629-1592 | 50488 ( ENGINE, GAS TURBINE, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-629-1592
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4135100 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-629-1592
| Characteristic | Specifications |
|---|---|
| FUEL TYPE | JET FUEL |
| POWER OUTPUT FOR WHICH DESIGNED | SHAFT |
| MOUNTING TYPE | AIRCRAFT |
| SPECIAL FEATURES | USED ON ENGINES 8-37 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F135PW600 STOVL ENGINE |