snapped during flight in say a Cherokee would that render the aircraft uncontrollable about the lateral axis? Or would there be a degree of pitch control through the trim?
My guess is the rudder would stay in the full nose up or nose down position & no trim input would change that? and the only real chance of pitch control would be through throttle inputs (less throttle = lower nose attitude & vice versa).
Your thoughts please.
My guess is the rudder would stay in the full nose up or nose down position & no trim input would change that? and the only real chance of pitch control would be through throttle inputs (less throttle = lower nose attitude & vice versa).
Your thoughts please.
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