Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-063-7324 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: 709451CL9, 2840-00-063-7324, 00-063-7324, 2840000637324, 000637324
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 19, 1972 | 00-063-7324 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-063-7324
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 709451CL9 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-063-7324
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 1.919 INCHES NOMINAL |
| OVERALL WIDTH | 2.020 INCHES NOMINAL |
| SPECIAL FEATURES | 1.188-1.198 SQ IN. FLOW AREA |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TF30 AIRCRAFT ENGINE |