In my case left wing , requires about 3/8 inch deflection to maintain level flight with ball centered, no leg or wheel fairings. There is little change in deflection with speed.
My thoughts, left roll due to less lift on left wing, so... how is this corrected with vertical aileron position or squeezing trailing edge of aileron.
I am assuming that either of the above options simply allow the aileron to fly in the 3/8 inch low position without any stick pressure.
I would like to fly level with the tip, aileron and flaps in trail without any deflections.
If this is correct then it would appear that I have to adjust the wing incidence or tip twist.
What I have found is a .1 degree higher incidence on the right wing and approx a 1/4 inch droop in the right tip relative to the left tip. Ailerons are equal vertically, there is no twist in the ailerons and flaps. I did go through the Vans check list for heavy wing.
Is this small amount of difference in incidence or tip droop enough to cause this amount of aileron deflection ?
My thoughts, left roll due to less lift on left wing, so... how is this corrected with vertical aileron position or squeezing trailing edge of aileron.
I am assuming that either of the above options simply allow the aileron to fly in the 3/8 inch low position without any stick pressure.
I would like to fly level with the tip, aileron and flaps in trail without any deflections.
If this is correct then it would appear that I have to adjust the wing incidence or tip twist.
What I have found is a .1 degree higher incidence on the right wing and approx a 1/4 inch droop in the right tip relative to the left tip. Ailerons are equal vertically, there is no twist in the ailerons and flaps. I did go through the Vans check list for heavy wing.
Is this small amount of difference in incidence or tip droop enough to cause this amount of aileron deflection ?