Part Details | AIRCRAFT GAS TURBINE ENGINE COMBUSTION CHAMBER
2840-01-305-2288 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: 1602M30G02, 1602M30, 2840-01-305-2288, 01-305-2288, 2840013052288, 013052288
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 02, 1989 | 01-305-2288 | 50337 ( CHAMBER, COMBUSTION, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-305-2288
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1602M30G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1602M30 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-305-2288
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| OVERALL LENGTH | 7.392 INCHES MINIMUM AND 7.527 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F110-4, FIGURE 67, INDEX 6, USED ON THE COMBUSTION DIFFUSER NOZZLE, HPT SHROUD |
| END ITEM IDENTIFICATION | ACFT ENG F110 |