Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-114-4775 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: 6009T46G08, 2840-01-114-4775, 01-114-4775, 2840011144775, 011144775
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 17, 1981 | 01-114-4775 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-114-4775
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6009T46G08 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-114-4775
| Characteristic | Specifications |
|---|---|
| DIAMETER | 16.855 INCHES MINIMUM AND 16.859 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG J-85 |