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Designer Jean-Rene Lepage, the Canadian engineer who developed the aircraft over a period of three years, realised that the four-stroke was fairly heavy for its rated horsepower and therefore designed the aircraft with long wings and a relatively short nose. Ultravia’s publicity material describes Le Pelican as ‘a new ultralight respectful of aircraft tradition’ and is powered by a four-stroke twin-cylinder Briggs & Stratton engine. Aircraft-grade aluminium used for structural components. Covering of framework and wing is Dacron. Engine mounted below wing driving tractor propeller. Aluminium-tube framework with glass-fibre nose and fabric covering, partially enclosed (total enclosure optional).
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Push-right go-right tailwheel steering connected to yaw control. Undercarriage has three wheels in taildragger formation axle-Flex suspension on main wheels. Wing braced from below by struts wing profile double-surface. Pitch control by elevator on tail yaw control by fully flying rudder roll control by 40%-span ailerons control inputs through stick for pitch/roll and pedals for yaw. Wing has unswept leading and trailing edges, and constant chord cruciform tail. Single-seat single-engined high-wing monoplane with conventional three-axis control. –-PLANS-AND-INFORMATION-SET-FOR-HOMEBUILD-AIRCRAFT-–-SIMPLE-AND-CHEAP-1-SEAT-TUBE-FABRIC-1.mp4