Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-673-2210 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: 798452CL10, 781252CL10, 565752CL10, 446952CL10, 422552CL10, 2840-00-673-2210, 00-673-2210, 2840006732210, 006732210
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1961 | 00-673-2210 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-673-2210
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 798452CL10 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 781252CL10 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 565752CL10 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 446952CL10 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 422552CL10 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-673-2210
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 2.482 INCHES NOMINAL |
| SPECIAL FEATURES | WAS VANE,TURBINE NOZZLE,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG32 IND1 |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE 2.402-2.424 SQ. IN. |