Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-01-247-6295 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: 9995M14G08, 9995M14G07, 9995M14G05, 2840-01-247-6295, 01-247-6295, 2840012476295, 012476295
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 09, 1987 | 01-247-6295 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-247-6295
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9995M14G08 | 58828 | CFM INTERNATIONAL, INC. |
| 9995M14G07 | 58828 | CFM INTERNATIONAL, INC. |
| 9995M14G05 | 58828 | CFM INTERNATIONAL, INC. |
Technical Data | NSN 2840-01-247-6295
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | REWORKED TO 9995M14G15 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT.ENG. F108 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | TURBINE NOZZLE ASSY-HIGH PRESSURE |