Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-106-2593 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: 111R112P25, 111R112P25, 108R815P1, 108R815P1, 111R112P25, 111R112P19, 111R112P10, 2840-01-106-2593, 01-106-2593, 2840011062593, 011062593
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 14, 1981 | 01-106-2593 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-106-2593
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 111R112P25 | 3204A | BLADES TECHNOLOGY LTD |
| 111R112P25 | S0635 | BLADES TECHNOLOGY LTDDBA ISCAR BLADES LTD. - FORMERLY |
| 108R815P1 | 24446 | GENERAL ELECTRIC COMPANY |
| 108R815P1 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 111R112P25 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 111R112P19 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 111R112P10 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-106-2593
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| STAGE NUMBER | 7 |
| OVERALL LENGTH | 4.138 INCHES MINIMUM AND 4.140 INCHES MAXIMUM |
| OVERALL WIDTH | 0.491 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.010 INCHES MINIMUM AND 0.020 INCHES MAXIMUM |
| END ITEM IDENTIFICATION | ACFT ENG J79 |