Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-01-317-1934 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: 4076395, 4075985, 4075975, 4075855, 2840-01-317-1934, 01-317-1934, 2840013171934, 013171934
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 24, 1990 | 01-317-1934 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-317-1934
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4076395 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4075985 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4075975 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4075855 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-317-1934
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 5 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F100PW0229 |
