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THE MAIN GEAR DAMPER IS INSTALLED ON THE TORSION LINKS OF EACH MAIN LANDING GEAR. THE MAIN GEAR DAMPER ASSEMBLEY INCLUDES A PISTON IN A HOUSING, WITH AN ATTACHED MANIFOLD AND COMPENSATOR WITH ITS OWN PISTON IN A HOUSING. THE UNIT IS CONNECTED TO THE HYDRAULIC SYSTEM. THE MOTION OF THE PISTONS IN THE UNIT INCREASES THE RATE AT WHICH THE INNER CYLINDER COMES TO A STOP AS IT TRIES TO TURN FROM SIDE TO SIDE COMPARED TO THE OUTER CYLINDER. THIS ACTION HELPS PREVENT UNWANTED VIBRATION OF THE MAIN LANDING GEAR DURING LANDING. MADE FROM STEEL. DIMENSIONS (APPROXIMATE) (L) 6 INCHES X (H) 6 INCHES X (W) 6 INCHES WEIGHT ((APPROXIMATE): 6 POUNDS. FOR USE SOLELY IN CIVIL AIRCRAFT.

AIRCRAFT LANDING GEAR MECHANISM. EXCLUDING THE WHEELS AND TYRES. FOR USE IN CIVIL AIRCRAFT OF AN UNLADEN WEIGHT OF OVER 8000 KG.

PROPRIETARY TITANIUM PART USED IN THE MANUFACTURE OF AIRCRAFT LANDING AND BRAKING SYSTEMS. THIS PART IS MANUFACTURED TO PRECISE SPECIFICATION AND CANNOT BE USED IN ANY OTHER APPLICATION OTHER THAN THAT OF AIRCRAFT LANDING AND BRAKING SYSTEMS. USED ON THE AIRBUS A330 AND A340 ONLY.

PROPRIETARY TITANIUM PART USED IN THE MANUFACTURE OF AIRCRAFT LANDING AND BRAKING SYSTEMS. THIS PART IS MANUFACTURED TO PRECISE SPECIFICATION AND CANNOT BE USED IN ANY OTHER APPLICATION OTHER THAN THAT OF AIRCRAFT LANDING AND BRAKING SYSTEMS. USED ON THE AIRBUS A330 AND A340 ONLY.

PROPRIETARY TITANIUM PART USED IN THE MANUFACTURE OF AIRCRAFT LANDING AND BRAKING SYSTEMS. THIS PART IS MANUFACTURED TO PRECISE SPECIFICATION AND CANNOT BE USED IN ANY OTHER APPLICATION OTHER THAN THAT OF AIRCRAFT LANDING AND BRAKING SYSTEMS. USED ON THE BOEING 787 ONLY.