greetings! vic steelhammer here.
i've had similar problems with my 14-19 N522A, although it is right wing heavy. the structure has not seen any serious damage in it's life (that i can see) and the left and right wings appear to be rigged very close to each other. i notice that the aileron linkages have a little slop in them, so that will be cinched up at annual this year with new hardware and rigging. the factory says "...just droop the flaps as needed" but this seems crude and inefficient to me. i checked the tail rigging best i could, but it's difficult to measure accurately. there is little or no information on the flying wire tensions that i could find. i wonder if the tail being twisted could have any more effect than a drooped flap as the moment arm of the horizontal is less than the flap (flaps extend farther spanwise than the horizontal).
my guess is that since the wings are not adjustable (like a piper or stinson) that we're limited to some sort of aileron trim tab (assuming the ailerons aren't warped). there have been some good articles on rigging in sport aviation in the last couple of years. make sure the ball is centered and then trim the roll. anyone have any other suggestions?
blue skies to all,
vic & N522A