Part Details | AIRCRAFT GAS TURBINE ENGINE INNER AUGMENTOR NOZZLE SECTION
2840-01-308-4465 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: 4071142, 2840-01-308-4465, 01-308-4465, 2840013084465, 013084465
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 29, 1989 | 01-308-4465 | 53241 ( AUGMENTOR NOZZLE SECTION, INNER, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-308-4465
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4071142 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-308-4465
| Characteristic | Specifications |
|---|---|
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F100 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |