Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-107-2930 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: 111R114P13, 111R114P13, 111R114P13, 2840-01-107-2930, 01-107-2930, 2840011072930, 011072930
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 03, 1981 | 01-107-2930 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-107-2930
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 111R114P13 | 3204A | BLADES TECHNOLOGY LTD |
| 111R114P13 | S0635 | BLADES TECHNOLOGY LTDDBA ISCAR BLADES LTD. - FORMERLY |
| 111R114P13 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-107-2930
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| OVERALL LENGTH | 1.906 INCHES MINIMUM AND 1.908 INCHES MAXIMUM |
| OVERALL WIDTH | 0.388 INCHES NOMINAL |
| END ITEM IDENTIFICATION | ACFT ENG J79 |