Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-01-447-2847 A stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle.
Alternate Parts: 9547M26G07, 2840-01-447-2847, 01-447-2847, 2840014472847, 014472847
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 31, 1997 | 01-447-2847 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-447-2847
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9547M26G07 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-447-2847
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| OVERALL LENGTH | 31.500 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F110GE129 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | NOZZLE ASSEMBLY,HIGH PRESSURE TURBINE STATOR |