Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-073-0590 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: K326P10, 2840-01-073-0590, 01-073-0590, 2840010730590, 010730590
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 08, 1979 | 01-073-0590 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-073-0590
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| K326P10 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-073-0590
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| STAGE NUMBER | 13 |
| OVERALL LENGTH | 1.891 INCHES NOMINAL |
| OVERALL WIDTH | 0.941 INCHES NOMINAL |
| OVERALL HEIGHT | 0.259 INCHES NOMINAL |
| SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF39-GE1C |