Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-013-1967 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: 6004T01P33, 2840-01-013-1967, 01-013-1967, 2840010131967, 010131967
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 27, 1975 | 01-013-1967 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-013-1967
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6004T01P33 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-013-1967
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 1.997 INCHES MINIMUM AND 2.023 INCHES MAXIMUM |
| OVERALL HEIGHT | 2.515 INCHES MINIMUM AND 2.555 INCHES MAXIMUM |
| DIAMETER | 17.040 INCHES MINIMUM AND 17.050 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-J85-94; TO BE RENAMED NOZZLE ASSY,TURBINE,GAS TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ENGINE,AIRCRAFT,TURBOJET,MODEL NO. J85-GE-21 |