We were preflighting a Cessna 172G and noticed that when the aileron on the left side was aligned to the flap the right side was roughly an inch below the flap edge, and the control wheel is straight. If the aileron s are manually balanced left to right they droop a bit more than a half inch and the control wheel is about 29 degrees right.
I do not remember seeing this on a 172. Is this within limits? My concern was mostly about pushing tip stall as this effectively removes the washout. How much is too much?
Thanks!
I do not remember seeing this on a 172. Is this within limits? My concern was mostly about pushing tip stall as this effectively removes the washout. How much is too much?
Thanks!