NSN 2840-00-086-5111
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-086-5111 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: 446953CL2, 413853CL2, 565853CL2, 2840-00-086-5111, 00-086-5111, 2840000865111, 000865111
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-086-5111 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-086-5111
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 446953CL2 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 413853CL2 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 565853CL2 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-086-5111
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 2.035 INCHES MINIMUM AND 2.045 INCHES MAXIMUM |
| 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 2.948-2.963 SQ IN |