Part Details | AIRCRAFT TURBINE ENGINE TURBINE BLADE DAMPER
2840-01-509-0326 A device used to reduce high cycle fatigue on a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. It also acts as a seal. It may be of various shapes and cross sections.
Alternate Parts: 6080T32P21, 2840-01-509-0326, 01-509-0326, 2840015090326, 015090326
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 10, 2003 | 01-509-0326 | 50557 ( DAMPER, TURBINE BLADE, AIRCRAFT TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-509-0326
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6080T32P21 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-509-0326
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| END ITEM IDENTIFICATION | T700-GE-701D ENGINE FOR UH-60 BLACKHAWK AND AH-64 APACHE HELICOPTER |