Part Details | AIRCRAFT TURBINE ENGINE TURBINE BLADE DAMPER
2840-01-368-6235 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: 1676M18G05, 1676M18G05, 2840-01-368-6235, 01-368-6235, 2840013686235, 013686235
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 05, 1992 | 01-368-6235 | 50557 ( DAMPER, TURBINE BLADE, AIRCRAFT TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-368-6235
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1676M18G05 | 60168 | ENGINETICS CORPORATIONDBA ENGINETICS AERO SPACE |
| 1676M18G05 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-368-6235
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | GOES ON THE 4TH AND 5TH BEARING OIL SUPPLY; REDUCES VIBRATION WHEN IN OPERATION; SS 2840-01-358-7173 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110-GE-100 AIRCRAFT ENGINE |