Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-089-2764 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: 37E501086P118, 2840-01-089-2764, 01-089-2764, 2840010892764, 010892764
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 29, 1980 | 01-089-2764 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-089-2764
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 37E501086P118 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-089-2764
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 4.510 INCHES NOMINAL |
| OVERALL WIDTH | 1.238 INCHES MINIMUM AND 1.242 INCHES MAXIMUM |
| SPECIAL FEATURES | 0.251-0.253 IN. DIA OF 1 HOLE |
| END ITEM IDENTIFICATION | ACFT ENG J85 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE,TURBINE ENGINE |