Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-199-7390 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: 1317M71P04, 2840-01-199-7390, 01-199-7390, 2840011997390, 011997390
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 25, 1985 | 01-199-7390 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-199-7390
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1317M71P04 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-199-7390
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | LOCK |
| OVERALL LENGTH | 9.140 INCHES NOMINAL |
| DIAMETER | 2.368 INCHES NOMINAL |
| SPECIAL FEATURES | 2ND END WIDTH 2.174; 2 GROOVES 0.300-0.310 DEEP,0.218-0.222 WIDE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110 ACFT ENGINE |