RE: Spad to the Bone Dominator Problem
Thanks, Clean, for the full scale input.
Hi norbon
Have you checked the wing incidence? Your "squirley" description points in that direction. Mr.Clean pointed to that above when he suggested shimming up the wing trailing edge. If you don't have an incidence meter try this: view the wing end and draw an imaginary line from the leading edge (LE) to the center of the trailing edge (TE) thickness. This imaginary line must be parallel to the fuselage. About a 7/16" shim under the TE is not uncommon.