Part Details | AIRCRAFT GAS TURBINE ENGINE INNER AUGMENTOR NOZZLE SECTION
2840-01-382-3498 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: 9539M85G06, 9538M17G03, 2840-01-382-3498, 01-382-3498, 2840013823498, 013823498
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 01, 1993 | 01-382-3498 | 53241 ( AUGMENTOR NOZZLE SECTION, INNER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-382-3498
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9539M85G06 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9538M17G03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-382-3498
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| OVERALL LENGTH | 13.200 INCHES NOMINAL |
| SPECIAL FEATURES | 2J-F110-4; FIG 2-78/2-73 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | AIRCRAFT ENGINE F100 GE-129 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FLAP, PRIMARY |