Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-01-243-2541 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: 9995M14G11, 9995M14G04, 2840-01-243-2541, 01-243-2541, 2840012432541, 012432541
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 23, 1986 | 01-243-2541 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-243-2541
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9995M14G11 | 58828 | CFM INTERNATIONAL, INC. |
| 9995M14G04 | 58828 | CFM INTERNATIONAL, INC. |
Technical Data | NSN 2840-01-243-2541
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | REPLACED BY 9995M14G11 REWORKED TO 9995M14G17 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT.ENG. F108 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | TURBINE NOZZLE ASSY-HIGH PRESSURE |