Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-422-7703 A single 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.
Alternate Parts: 1881M21P02, 1881M21P01, 2840-01-422-7703, 01-422-7703, 2840014227703, 014227703
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 07, 1995 | 01-422-7703 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-422-7703
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1881M21P02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1881M21P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-422-7703
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 2.515 INCHES MINIMUM AND 2.535 INCHES MAXIMUM |
| SPECIAL FEATURES | MATL RENE N5 |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$ACZCJ$$AABHP$$AFEAT |
| END ITEM IDENTIFICATION | F101-GE-102 AIRCRAFT GAS TURBINE ENGINE |