Features

• Very small additional weight
• Very small additional aerodynamic cross section
• No consequences in case of mechanical failure of the hydraulic cylinder
• The system is based on simple and rugged mechanics
• The sophisticated aspects are related to the wheel synchronization, active during ground operation only and easily made redundant

Additional Features

• The system allows the pilot to rotate the wheels before touch down for testing
• In emergencies, the aircraft can be displaced to abandon a finger in case of danger (eg fire) or to free an area

The present document contains proprietary information and it is patent pending. An Italian application has been filed on September 10th, 2009 #BS2009A000165 - All content © Mario Gaia 2010.