Part Details | AIRCRAFT GAS TURBINE ENGINE
2840-01-475-2552 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: 9546M10G01, 2840-01-475-2552, 01-475-2552, 2840014752552, 014752552
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 26, 2000 | 01-475-2552 | 50488 ( ENGINE, GAS TURBINE, AIRCRAFT ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-475-2552
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9546M10G01 | 58828 | CFM INTERNATIONAL, INC. |
Technical Data | NSN 2840-01-475-2552
| Characteristic | Specifications |
|---|---|
| FUEL TYPE | JET FUEL |
| POWER OUTPUT FOR WHICH DESIGNED | PNEUMATIC/SHAFT |
| MOUNTING TYPE | ANY ACCEPTABLE |
| REFERENCE DATA AND LITERATURE | 2J-F100-4 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110-100B |