Part Details | AIRCRAFT GAS TURBINE ENGINE INNER AUGMENTOR NOZZLE SECTION
2840-01-443-5839 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: 5113T54P02, 2840-01-443-5839, 01-443-5839, 2840014435839, 014435839
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 14, 1997 | 01-443-5839 | 53241 ( AUGMENTOR NOZZLE SECTION, INNER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-443-5839
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5113T54P02 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-443-5839
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 19.380 INCHES NOMINAL |
| SPECIAL FEATURES | NAVAIR A1-F414A-IPB-400, FIG 066, INDEX 30 |
| END ITEM IDENTIFICATION | GE F414-400 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FLAP,SECONDARY-VARIABLE EXHAUST NOZZLE |