Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE
2840-01-528-3440 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: 5128T69P06, 2840-01-528-3440, 01-528-3440, 2840015283440, 015283440
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 10, 2005 | 01-528-3440 | 50531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-528-3440
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5128T69P06 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-528-3440
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | UN-GROUND COMPRESSOR ROTOR BLADES |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TURBO PROP ENGINES (T58) |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE,STAGE 4 LOCKER |