Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-00-944-3276 A 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. The assembled item forms a complete circle.
Alternate Parts: 111R643G03, 2840-00-944-3276, 00-944-3276, 2840009443276, 009443276
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 09, 1966 | 00-944-3276 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-944-3276
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 111R643G03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-944-3276
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 24.000 INCHES NOMINAL |
| OVERALL WIDTH | 12.000 INCHES NOMINAL |
| OVERALL HEIGHT | 12.000 INCHES NOMINAL |
| SPECIAL FEATURES | THIS TURBINE NOZZLE ASSY HAS A CRITICAL TOLERANCE,FIT RESTRICTION,AND APPLICATION |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| REFERENCE DATA AND LITERATURE | 2J-J79-64 FIG 28 IND1 |
| END ITEM IDENTIFICATION | ACFT ENG J79, J85, T58, T64 |