Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-00-999-3295 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: 730792, 704282, 512272, 2840-00-999-3295, 00-999-3295, 2840009993295, 009993295
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 26, 1966 | 00-999-3295 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-999-3295
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 730792 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 704282 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 512272 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-999-3295
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 2.495 INCHES MINIMUM AND 2.530 INCHES MAXIMUM |
| DIAMETER | 27.759 INCHES MINIMUM AND 27.763 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| PRECIOUS MATERIAL | GOLD |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |