Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-347-0820 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: 1522M85G01, 1522M85, 2840-01-347-0820, 01-347-0820, 2840013470820, 013470820
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 16, 1991 | 01-347-0820 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-347-0820
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1522M85G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1522M85 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-347-0820
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 2.475 INCHES NOMINAL |
| DIAMETER | 30.180 INCHES MINIMUM AND 30.220 INCHES MAXIMUM |
| END ITEM IDENTIFICATION | ACFT ENG F110 |