Part Details | AIRCRAFT TURBINE ENGINE TURBINE BLADE DAMPER
2840-01-444-6529 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: 1807M27G03, 1807M27, 2840-01-444-6529, 01-444-6529, 2840014446529, 014446529
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 13, 1997 | 01-444-6529 | 50557 ( DAMPER, TURBINE BLADE, AIRCRAFT TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-444-6529
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1807M27G03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1807M27 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-444-6529
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| SPECIAL FEATURES | ORIGNAL NAME DAMPER ASSEMBLY,HIGH PRESSURE TURBINE ROTOR-STAGE 1. G03 ADDED TO PART NUMBER PER CID 219639. THIS ITEM IS PART OF THE HT90 MOD FOR THE TF39 ENGING |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |