Part Details | AIRCRAFT GAS TURBINE ENGINE INNER AUGMENTOR NOZZLE SECTION
2840-01-616-1301 A rigid item designed to help direct the flow of hot gases from an AFTERBURNER,TURBINE ENGINE. It is an integral part of a NOZZLE,AUGMENTOR EXHAUST, AIRCRAFT GAS TURBINE ENGINE. The item is to the rear of and hinged to an AUGMENTOR NOZZLE SECTION,CONVERGENT, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 9539M85G12, 2840-01-616-1301, 01-616-1301, 2840016161301, 016161301
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 02, 2013 | 01-616-1301 | 53241 ( AUGMENTOR NOZZLE SECTION, INNER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-616-1301
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9539M85G12 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-616-1301
| Characteristic | Specifications |
|---|---|
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110-GE, 129 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FLAP, EXHAUST NOZZLE-PRIMARY |