Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-317-1932 A single 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.
Alternate Parts: 6068T31G06, 2840-01-317-1932, 01-317-1932, 2840013171932, 013171932
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 24, 1990 | 01-317-1932 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-317-1932
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6068T31G06 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-317-1932
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| STAGE NUMBER | 2 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 2.430 INCHES NOMINAL |
| OVERALL HEIGHT | 4.578 INCHES NOMINAL |
| END ITEM IDENTIFICATION | USED ON GE-701C ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | NOZZLE,TURBINE,TURBINE ENGINE |