Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-106-2589 An item mounted on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the compressor section of an ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: 111R109P7, 111R109P7, 111R109P4, 108B812P1, 111R109P7, 2840-01-106-2589, 01-106-2589, 2840011062589, 011062589
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 14, 1981 | 01-106-2589 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-106-2589
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 111R109P7 | 3204A | BLADES TECHNOLOGY LTD |
| 111R109P7 | S0635 | BLADES TECHNOLOGY LTDDBA ISCAR BLADES LTD. - FORMERLY |
| 111R109P4 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 108B812P1 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 111R109P7 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-106-2589
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 7.389 INCHES NOMINAL |
| OVERALL WIDTH | 2.084 INCHES MINIMUM AND 2.094 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.010 INCHES MINIMUM AND 0.020 INCHES MAXIMUM |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABMK$$AABPX$$ACZBJ |
| END ITEM IDENTIFICATION | ACFT ENG J79 |