Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-01-420-0654 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: 6894101, 2840-01-420-0654, 01-420-0654, 2840014200654, 014200654
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 05, 1995 | 01-420-0654 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-420-0654
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6894101 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-420-0654
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 2.927 INCHES NOMINAL |
| SPECIAL FEATURES | MATERIAL COATING THE MAIN CHANGE TO GIVE LONGER LIFE AND DURABILITY |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG T56-7B |