Lightweight aircraft

Details Lightweight aircraft Lightweight aircraft

B - Operations, Transporting

64

C

244/14

B64C 39/00 (2006.01) B64C 31/028 (2006.01)

Patent

CA 1144134

Abstract of the Disclosure An ultralight aircraft has a single stick three- axis aerodynamic control, twin engined power control, wing- and tail-mounted ailerons, an inverted V-tail and wide span wings with upturned tips.

363440

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