Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-339-7016 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: 2189814, 2189814, 2840-01-339-7016, 01-339-7016, 2840013397016, 013397016
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 28, 1991 | 01-339-7016 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-339-7016
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 2189814 | 1J4P3 | PARADIGM MANCHESTER INC.DBA PARADIGM PRECISION |
| 2189814 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-339-7016
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 9.732 INCHES MINIMUM AND 9.832 INCHES MAXIMUM |
| OVERALL WIDTH | 3.080 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.018 INCHES MINIMUM AND 0.021 INCHES MAXIMUM |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | NOZZLE,TURBINE,TURBINE ENGINE |