Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-444-7693 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: 1864M32G02, 2840-01-444-7693, 01-444-7693, 2840014447693, 014447693
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 15, 1997 | 01-444-7693 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-444-7693
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1864M32G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-444-7693
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 2.013 INCHES MINIMUM AND 2.087 INCHES MAXIMUM |
| OVERALL HEIGHT | 4.482 INCHES MINIMUM AND 4.505 INCHES MAXIMUM |
| DIAMETER | 34.568 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-TF39-4, FIG 62 IND 22; BOROSCOPE LOCATION; REPL P/N 9022M16G26; WHOLE NEW CONFIG BASED ON ECP 369, DCN 97-37; NEW MATL AND DESIGN CHANGES; NOT TO BE GRPD TO OLD CONFIG; WHEN OLD CONFIG COMES IN AND REPL BY TCTO KITS WITH NEW PARTS, OLD CONFIG IS THROWN AWAY, NOT MODIFIED, NOT I&SABLE; QTY 1 PER ASSY |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABKW$$AABMZ$$AFEAT |
| END ITEM IDENTIFICATION | TF-39 AIRCRAFT GAS TURBINE ENGINE |