Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER
2840-01-113-3785 The portion of an ENGINE, GAS TURBINE, AIRCRAFT in which fuel is burned. It may be an annular type in which the space between the circular inner and outer cylinders form the burning chamber or it may be the multi-arrangement can type in which separate can like burn cylinders are positioned in a circular arrangement within an inner and outer case.
Alternate Parts: 7012M89G11, 2840-01-113-3785, 01-113-3785, 2840011133785, 011133785
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 21, 1981 | 01-113-3785 | 50337 ( CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-113-3785
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 7012M89G11 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-113-3785
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | ENGINE MODEL J79-GE-10 |