Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-349-0428 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: 30913821, 3091382-1, 2840-01-349-0428, 01-349-0428, 2840013490428, 013490428
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 20, 1991 | 01-349-0428 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-349-0428
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3091382-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-349-0428
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 1.240 INCHES MINIMUM AND 1.260 INCHES MAXIMUM |
| DIAMETER | 12.428 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | PACER DAWN |