Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-00-908-6065 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: 730670, 704170, 512270, 2840-00-908-6065, 00-908-6065, 2840009086065, 009086065
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1960 | 00-908-6065 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-908-6065
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 730670 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 704170 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 512270 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-908-6065
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 2.612 INCHES MINIMUM AND 2.734 INCHES MAXIMUM |
| DIAMETER | 27.720 INCHES MINIMUM AND 27.740 INCHES MAXIMUM |
| SPECIAL FEATURES | 19.320-19.330 IN. ID |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| PRECIOUS MATERIAL | GOLD |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENG |