Part Details | AIRCRAFT GAS TURBINE ENGINE INNER AUGMENTOR NOZZLE SECTION
2840-01-443-4137 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: 5103T26P01, 2840-01-443-4137, 01-443-4137, 2840014434137, 014434137
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 10, 1997 | 01-443-4137 | 53241 ( AUGMENTOR NOZZLE SECTION, INNER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-443-4137
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5103T26P01 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-443-4137
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | GE F414-4000 ENGINE |