Part Details | TURBINE ENGINE AFTERBURNER
2840-01-325-8015 A chamber in which additional fuel is injected into, the exhaust gases, and reheating the gases to develop increased thrust. It consists of combustion area, flame holders, injection nozzles and an exhaust ejector.
Alternate Parts: 9521M23G08, 2840-01-325-8015, 01-325-8015, 2840013258015, 013258015
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 11, 1990 | 01-325-8015 | 60031 ( AFTERBURNER, TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-325-8015
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9521M23G08 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-325-8015
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | AFTERBURNER |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110GE100 AIRCRAFT ENGINE |