Part Details | AIRCRAFT GAS TURBINE ENGINE
2840-01-529-1291 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: CF680C2A2, CF6-80C2A2, 2840-01-529-1291, 01-529-1291, 2840015291291, 015291291
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 05, 2005 | 01-529-1291 | 50488 ( ENGINE, GAS TURBINE, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-529-1291
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| CF6-80C2A2 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-529-1291
| Characteristic | Specifications |
|---|---|
| FUEL TYPE | JET FUEL |
| MOUNTING TYPE | AIRCRAFT |
| OVERALL LENGTH | 168.000 INCHES NOMINAL |
| SPECIAL FEATURES | 106 IN. MAX. DIA.; HIGH-BYPASS TURBOFAN; 53.500 MAX POWER AT SEA LEVEL |
| END ITEM IDENTIFICATION | A310 TRANSPORT AIRCRAFT |