Part Details | AIRCRAFT GAS TURBINE ENGINE INNER AUGMENTOR NOZZLE SECTION
2840-01-381-5393 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: 5051M72G09, 1465M50G08, 2840-01-381-5393, 01-381-5393, 2840013815393, 013815393
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 18, 1993 | 01-381-5393 | 53241 ( AUGMENTOR NOZZLE SECTION, INNER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-381-5393
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5051M72G09 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1465M50G08 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-381-5393
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| OVERALL LENGTH | 22.090 INCHES MINIMUM AND 22.170 INCHES MAXIMUM |
| SPECIAL FEATURES | 2J-F110-4, FIG 2-78/2-73 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110GE129 AIRCRAFT ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FLAP, EXHAUST NOZZLE-DIVERGENT |