Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-447-2509 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: K019G03, K019G02, K019G01, 2840-01-447-2509, 01-447-2509, 2840014472509, 014472509
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 30, 1997 | 01-447-2509 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-447-2509
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| K019G03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| K019G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| K019G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-447-2509
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 1.472 INCHES NOMINAL |
| SPECIAL FEATURES | MODIFIED BLADE HAS TUNGSTEN CARBIDE WEAR COATING ON THE MIDSPAN SHROUDS AND REPLACES P/NS K159P01, P02, P04, P07 WITH A BRAZED ON CARBALOY WEAR PAD FOR INCREASED WEAR LIFE |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | TF-39 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME BLADE,COMPRESSOR ROTOR |