Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-038-3316 An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: 37E501086P112, 2840-01-038-3316, 01-038-3316, 2840010383316, 010383316
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 03, 1977 | 01-038-3316 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-038-3316
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 37E501086P112 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-038-3316
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | LOCK |
| SPECIAL FEATURES | T.O. 2J-J85-54; 31 BLADES |
| END ITEM IDENTIFICATION | AIRCRAFT ENGINE,J85-GE-5,-17,-13 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE,TURBINE ENGINE |