Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-318-4806 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: 6900T83G01, 2840-01-318-4806, 01-318-4806, 2840013184806, 013184806
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 19, 1990 | 01-318-4806 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-318-4806
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6900T83G01 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-318-4806
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 2 |
| BLADE ATTACHMENT METHOD | LOCK |
| OVERALL LENGTH | 16.733 INCHES MINIMUM AND 16.737 INCHES MAXIMUM |
| SPECIAL FEATURES | AIR IMPINGMENT STARTER |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J85-5J/13D ENGINE |