Part Details | AIRCRAFT GAS TURBINE ENGINE
2840-01-266-0346 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: 6046T10G01, F404GE400, F404-GE-400, 2840-01-266-0346, 01-266-0346, 2840012660346, 012660346
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 20, 1987 | 01-266-0346 | 50488 ( ENGINE, GAS TURBINE, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-266-0346
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6046T10G01 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| F404-GE-400 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-266-0346
| Characteristic | Specifications |
|---|---|
| POWER OUTPUT FOR WHICH DESIGNED | SHAFT |
| MOUNTING TYPE | AIRCRAFT |
| SPECIAL FEATURES | TYPE/MODEL DESINGATION F404-GE-400; REFERENCE DATA AND LITERATURE GE ECP G404-C-42, PAGE 11 |