NSN 2840-00-898-7574
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-898-7574 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: 446953CL4, 413853CL4, 565853CL4, 2840-00-898-7574, 00-898-7574, 2840008987574, 008987574
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
28 | JAN 01, 1962 | 00-898-7574 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-898-7574
Part Number | Cage Code | Manufacturer |
---|---|---|
446953CL4 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
413853CL4 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
565853CL4 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-898-7574
Characteristic | Specifications |
---|---|
ENGINE SECTION LOCATION | TURBINE |
STAGE NUMBER | 3 |
OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
SPECIAL FEATURES | WAS VANE,TURBINE NOZZLE,TURBINE ENGINE |
CRITICALITY CODE JUSTIFICATION | AGAV |
REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG32 IND14 |
END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE 2.978-2.993 SQ IN |