Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-317-8323 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: 6029T45G12, 2840-01-317-8323, 01-317-8323, 2840013178323, 013178323
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 06, 1990 | 01-317-8323 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-317-8323
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6029T45G12 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-317-8323
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 2.013 INCHES NOMINAL |
| OVERALL HEIGHT | 2.535 INCHES NOMINAL |
| DIAMETER | 17.045 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-J85-94; TO BE RENAMED NOZZLE ASSY,TURBINE,GAS TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J85-GE-21B AIRCRAFT ENGINE |