Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-01-252-4095 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: P223P03, P223P01, P203P03, P223P03, P223P01, 2840-01-252-4095, 01-252-4095, 2840012524095, 012524095
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 01, 1987 | 01-252-4095 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-252-4095
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| P223P03 | 58828 | CFM INTERNATIONAL, INC. |
| P223P01 | 58828 | CFM INTERNATIONAL, INC. |
| P203P03 | 58828 | CFM INTERNATIONAL, INC. |
| P223P03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| P223P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-252-4095
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 3 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT.ENG. F108 |
