Part Details | AIRCRAFT GAS TURBINE ENGINE AUGMENTER EXHAUST NOZZLE
2840-01-155-9148 A compliment of several eyelet or flap type items that form a duct like end on an ENGINE, GAS TURBINE, AIRCRAFT. The eyelets are moved by hydraulic actuators to cause the opening to become larger or smaller. The changing of the opening size controls the thrust and temperature of the engine. This item is only used on engines with an AFTERBURNER, TURBINE ENGINE attached.
Alternate Parts: 4056264, 2840-01-155-9148, 01-155-9148, 2840011559148, 011559148
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 16, 1983 | 01-155-9148 | 50351 ( NOZZLE, AUGMENTER EXHAUST, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-155-9148
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4056264 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-155-9148
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | AFTERBURNER |
| OVERALL LENGTH | 20.610 INCHES MINIMUM AND 20.730 INCHES MAXIMUM |
| SPECIAL FEATURES | T. O. 2J-F100-24, FIG 147, IND 57. |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AFEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-24, FIG 87, IND 49 |
| END ITEM IDENTIFICATION | ACFT ENG F100/200 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | T.O. NAME NOZZLE SEGMENT ASSEMBLY, DIVERGENT AUGMENTOR |