Part Details | AIRCRAFT GAS TURBINE ENGINE OUTER AUGMENTOR NOZZLE SECTION
2840-01-357-1941 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,AUGMENTER EXHAUST,AIRCRAFT GAS TURBINE ENGINE. The item is external to the AUGMENTOR NOZZLE SECTION,CONVERGENT,AIRCRAFT GAS TURBINE ENGINE and the AUGMENTOR NOZZLE SECTION,INNER,AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 9538M95G05, 9538M95, 9538M24G04, 9538M24, 2840-01-357-1941, 01-357-1941, 2840013571941, 013571941
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 18, 1992 | 01-357-1941 | 53242 ( AUGMENTOR NOZZLE SECTION, OUTER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-357-1941
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9538M95G05 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9538M95 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9538M24G04 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9538M24 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-357-1941
| Characteristic | Specifications |
|---|---|
| MATERIAL | TITANIUM ALLOY |
| OVERALL LENGTH | 26.880 INCHES MINIMUM AND 26.990 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F110-GE-100 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | FLAP, EXHAUST NOZZLE-OUTER |