Light engine-powered aircraft with improved balance

摘要

The aircraft has a control rudder bar (201) with first and second pedals (281, 283) inducing control on a vertical pivoting board (304) opposite to control of third and fourth pedals (282, 284). A cockpit receives a unique seat arranged in a median plane of the aircraft by replacing first and second seats, and arranged in opposite to the second and third pedals, where the first and second seats are arranged side by side on the plane. An inversion device includes ball joints (295-298) and links (271-274) to selectively invert the controls applied to the board by the second and third pedals.