Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-106-2596 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: 111R113P25, 111R113P25, 111R113P25, 111R113P25, 111R113P25, 2840-01-106-2596, 01-106-2596, 2840011062596, 011062596
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 14, 1981 | 01-106-2596 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-106-2596
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 111R113P25 | 3204A | BLADES TECHNOLOGY LTD |
| 111R113P25 | S0635 | BLADES TECHNOLOGY LTDDBA ISCAR BLADES LTD. - FORMERLY |
| 111R113P25 | 68544 | COMPRESSOR COMPONENTS TEXTRON INCSUB OF TEXTRON INC |
| 111R113P25 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 111R113P25 | 06351 | MICROWAVE ENGINEERING CORPORATION |
Technical Data | NSN 2840-01-106-2596
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| STAGE NUMBER | 10 |
| OVERALL LENGTH | 2.750 INCHES MINIMUM AND 2.752 INCHES MAXIMUM |
| OVERALL WIDTH | 0.390 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.010 INCHES MINIMUM AND 0.020 INCHES MAXIMUM |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG J79 |