Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-444-6999 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: 1881M89G01, 2840-01-444-6999, 01-444-6999, 2840014446999, 014446999
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 14, 1997 | 01-444-6999 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-444-6999
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1881M89G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-444-6999
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 1.883 INCHES MINIMUM AND 1.888 INCHES MAXIMUM |
| OVERALL HEIGHT | 3.351 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-TF39-4, FIG 61, IND 2; ECP 369, DCN 97-37; 1.451 IN. BETWEEN NOZZLE AIR FLOW CAVITIES OC; 1.703 LENGTH OF NOZZLE FIN; 1.415 WIDTH OF NOZZLE FIN; REPL P/N 9082M95G15; NOT TO BE GRPED PER ECP/DCN; WHOLE NEW CONFIGURATION; AS THE OLD CONFIG IS REPLACED BY TCTO KITS WITH THE NEW ITEM, THE OLD CONFIG IS THEN THROWN AWAY |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABKW$$AFEAT |
| END ITEM IDENTIFICATION | TF-39 AIRCRAFT GAS TURBINE ENGINE |