Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-01-104-1685 A 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. The assembled item forms a complete circle.
Alternate Parts: 6041T41G09, 2840-01-104-1685, 01-104-1685, 2840011041685, 011041685
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 28, 1980 | 01-104-1685 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-104-1685
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6041T41G09 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-104-1685
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| DIAMETER | 17.040 INCHES MINIMUM AND 17.050 INCHES MAXIMUM |
| SPECIAL FEATURES | ORIG NAME NOZZLE,TURBINE,TURBINE ENGINE; MARK NOZZLE MECHANICAL AREA, AE 44.072-44.515 SQ IN. |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$AABMZ |
| END ITEM IDENTIFICATION | ACFT ENG J85 |