Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-200-8832 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: 1317M71P02, 2840-01-200-8832, 01-200-8832, 2840012008832, 012008832
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 10, 1985 | 01-200-8832 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-200-8832
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1317M71P02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-200-8832
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | LOCK |
| OVERALL LENGTH | 9.140 INCHES NOMINAL |
| OVERALL WIDTH | 3.368 INCHES NOMINAL |
| SPECIAL FEATURES | BOTTOM WIDTH,2ND END 2.174 IN.; 2 GROOVES NEAR BOTTOM 0.225 BY 0.220 IN.; MATL C50TF22 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110 ACFT ENGINE |