Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-962-1263 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: 799554CL6, 565854CL6, 495254CL6, 2840-00-962-1263, 00-962-1263, 2840009621263, 009621263
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1962 | 00-962-1263 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-962-1263
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 799554CL6 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 565854CL6 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 495254CL6 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-962-1263
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 4 |
| OVERALL LENGTH | 8.740 INCHES NOMINAL |
| OVERALL WIDTH | 2.390 INCHES NOMINAL |
| MATERIAL THICKNESS | 1.245 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-TF33-14, FIG 30, IND 19; 4.853-4.884 SQ IN |
| CRITICALITY CODE JUSTIFICATION | FEATG |
| END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | WAS VANE,TURBINE NOZZLE,TURBINE ENGINE |