Part Details | AIRCRAFT GAS TURBINE ENGINE
2840-01-513-2027 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: 3813881E, 381388-1E, 3813881, 381388-1, 2840-01-513-2027, 01-513-2027, 2840015132027, 015132027
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 19, 2003 | 01-513-2027 | 50488 ( ENGINE, GAS TURBINE, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-513-2027
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 381388-1E | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 381388-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-513-2027
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | USED ON AIRBUS A310 AIRCRAFT |