Part Details | AIRCRAFT TURBINE ENGINE TURBINE BLADE DAMPER
2840-01-444-6530 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: 1807M15G05, 1807M15, 2840-01-444-6530, 01-444-6530, 2840014446530, 014446530
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 13, 1997 | 01-444-6530 | 50557 ( DAMPER, TURBINE BLADE, AIRCRAFT TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-444-6530
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1807M15G05 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1807M15 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-444-6530
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 2 |
| SPECIAL FEATURES | ORIGINAL NAME DAMPER ASSEMBLY,HIGH PRESSURE TURBINE ROTOR-STAGE 2. ALSOPART NUMBER G05 ADDED PER CID 219639 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |