Part Details | AIRCRAFT GAS TURBINE ENGINE
2840-01-551-3591 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: 38007081, 3800708-1, 2840-01-551-3591, 01-551-3591, 2840015513591, 015513591
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 15, 2007 | 01-551-3591 | 50488 ( ENGINE, GAS TURBINE, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-551-3591
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3800708-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-551-3591
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | MODEL NUMBER 131-9(A) APU; PROVIDES POWER FOR AIRCRAFT SYSTEMS AND FOR ENGINE STARTING |
| END ITEM IDENTIFICATION | AIRCRAFT, AIRBUS, MODELS A318, A319, A320, AND A321 |