Part Details | AIRCRAFT GAS TURBINE ENGINE CONVERGENT AUGMENTOR NOZZLE SECTION
2840-01-562-8778 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 to the front of an AUGMENTOR NOZZLE SECTION,INNER,AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 432272901, 4322729-01, 2840-01-562-8778, 01-562-8778, 2840015628778, 015628778
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 24, 2008 | 01-562-8778 | 53240 ( AUGMENTOR NOZZLE SECTION, CONVERGENT, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-562-8778
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4322729-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-562-8778
| Characteristic | Specifications |
|---|---|
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F-119-PW-100 ENGINE ON F-22 AIRCFAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | NOZZLE-AUGMENTOR,CONVERGENT ASSEMBLY |