Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-00-966-8058 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: 730793, 704283, 476673, 2840-00-966-8058, 00-966-8058, 2840009668058, 009668058
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1962 | 00-966-8058 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-966-8058
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 730793 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 704283 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 476673 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-966-8058
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 2.350 INCHES MINIMUM AND 2.362 INCHES MAXIMUM |
| DIAMETER | 27.631 INCHES MINIMUM AND 27.641 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| PRECIOUS MATERIAL | GOLD |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |