posted on May, 1 2019 @ 12:00 AM
So there was a little more to this than originally reported. In late 2015 control laws were changed to improve air to ground transitions. This
resulted in cyclic sensitivity increasing 2.5x while in transition. During the accident, the aircraft detected weight coming off the wheels, and
shifted to in- transition mode on the flight controls. As they got airborne, there was a slight left roll, so the pilot input right roll to correct.
Instead, the aircraft rolled as much as 60 degrees right, resulting in the main rotors touching, snapping the blade tips off. The pilot attempted to
land quickly, and the landing gear collapsed, resulting in the pusher prop impacting the runway.
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