Part Details | TURBINE ENGINE AFTERBURNER
2840-01-440-4352 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: 9547M23G10, 2840-01-440-4352, 01-440-4352, 2840014404352, 014404352
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 13, 1997 | 01-440-4352 | 60031 ( AFTERBURNER, TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-440-4352
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9547M23G10 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-440-4352
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | AFTERBURNER |
| SPECIAL FEATURES | ECPFI120; P/N 9547M23G10 IS THE SAME AS THE 9547M23G07 EXCEPT THE G10 DELETES 5 DAMPER RING LINKS AND LINK ATTACHMENT PINS TO ELIMINATE THE WEAR PROBLEM |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$AFEAT |
| END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT GAS TURBINE ENGINE |