Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-317-1933 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: 6068T85G08, 6068T85G06, 2840-01-317-1933, 01-317-1933, 2840013171933, 013171933
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 24, 1990 | 01-317-1933 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-317-1933
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6068T85G08 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 6068T85G06 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-317-1933
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 2.395 INCHES NOMINAL |
| END ITEM IDENTIFICATION | USED ON GE-701C ENGINE |