Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-936-6722 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: 576754CL2, 576754CL2, 576754CL2, 576754CL2, 576754CL2, 2840-00-936-6722, 00-936-6722, 2840009366722, 009366722
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 08, 1967 | 00-936-6722 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-936-6722
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 576754CL2 | 3V257 | HOWMET CORPORATIONDIV HOWMET MACHINING |
| 576754CL2 | 99160 | THERM, INCORPORATED |
| 576754CL2 | 96965 | TURBINE AIRFOIL DESIGNS INC. |
| 576754CL2 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 576754CL2 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-936-6722
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | WAS VANE,TURBINE NOZZLE,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TF30 AIRCRAFT ENGINE |
