Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-01-485-9577 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: 1881M72G02, 2840-01-485-9577, 01-485-9577, 2840014859577, 014859577
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 12, 2001 | 01-485-9577 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-485-9577
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1881M72G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-485-9577
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 2 |
| REFERENCE DATA AND LITERATURE | 2J-TF39-4 |
| END ITEM IDENTIFICATION | TF39 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | MODULE-HIGH POWER TURBINE,ROTOR/STATOR |