Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-361-0123 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: 9942M44P04, 2840-01-361-0123, 01-361-0123, 2840013610123, 013610123
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 07, 1992 | 01-361-0123 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-361-0123
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9942M44P04 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-361-0123
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 3.130 INCHES MINIMUM AND 3.140 INCHES MAXIMUM |
| OVERALL WIDTH | 1.600 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F101 ACFT ENGINE |