Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-017-3439 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: 5900T51P01, 2840-01-017-3439, 01-017-3439, 2840010173439, 010173439
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 06, 1976 | 01-017-3439 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-017-3439
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5900T51P01 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-017-3439
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 1.649 INCHES MINIMUM AND 1.683 INCHES MAXIMUM |
| DIAMETER | 16.855 INCHES MINIMUM AND 16.859 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-J85-94, FIG 19, IND 20 |
| CRITICALITY CODE JUSTIFICATION | AABHP$$ACZBJ$$AABMZ$$ACZCJ$$AABHP |
| END ITEM IDENTIFICATION | J85-GE-21 AIRCRAFT ENGINE |