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Lets say were in a crosscontrolled skidded stall . We are banking left and decide to try and increase rate of turn by adding left rudder. we do not want to increase the bank angle so we keep it constant, by adding right aileron to counteract the left banking bi product from rudder. we than notice the nose of the plane is dropping so we use aft elevator untill the airplane stalls. Why is it that the airplane will roll towards the left wing?
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