NSN 2840-00-256-1081
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-256-1081 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: 799351CL20, 799351CL20, 799351CL20, 799351CL20, 799351CL20, 665951CL20, 536751CL20, 2840-00-256-1081, 00-256-1081, 2840002561081, 002561081
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
28 | JAN 12, 1972 | 00-256-1081 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-256-1081
Part Number | Cage Code | Manufacturer |
---|---|---|
799351CL20 | 3V257 | HOWMET CORPORATIONDIV HOWMET MACHINING |
799351CL20 | 26199 | JOHNSON TECHNOLOGY, INC. |
799351CL20 | 99160 | THERM, INCORPORATED |
799351CL20 | 96965 | TURBINE AIRFOIL DESIGNS INC. |
799351CL20 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
665951CL20 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
536751CL20 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-256-1081
Characteristic | Specifications |
---|---|
ENGINE SECTION LOCATION | TURBINE |
STAGE NUMBER | 1 |
SPECIAL FEATURES | 1.446-1.455 SQ. IN. FLOW AREA |
CRITICALITY CODE JUSTIFICATION | AGAV |
END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,TURBINE NOZZLE,TURBINE ENGINE |