Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-163-6701 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: 9395M67P01, 2840-01-163-6701, 01-163-6701, 2840011636701, 011636701
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 06, 1983 | 01-163-6701 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-163-6701
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9395M67P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-163-6701
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 5 |
| DIAMETER | 28.450 INCHES MINIMUM AND 28.465 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-TF39-4, FIG 67 IND 38; MADE ALTERNATE JAN 94 FOR MAINTENANCE ECONOMY PER T.O. 2J-TF39-4S-2 |
| CRITICALITY CODE JUSTIFICATION | AFEAT$$ACZCJ$$ACZBJ |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |