I understand the owner added some down thrust and the problem was solved, he then adjusted the length of the elevator push rod so the inside/outside turn rates were the same.
Can anybody explain, aerodynamically, how adding some down thrust cured the problem of floating too high on both upright and inverted.
I'm happy for the owner!
Stability. My guess is that the airplane has some built-in "up'stabilizer, so putting a constant torque on it forces it to operate to keep the same loading for normal near=level flight control motion. It is greatly exacerbated with a "flat stab", adding a pointy leadins edge reduces the problem.
My guess would be, without having seen it, that the airplane has a tiny amount of "up" stabilizer, which causes it to be unstable around neutral, just like many prior examples, and pushing outside the dead zone around neutral avoids the issue. If it had a removable tail, I would suggest a maybe .010-.015 shim under the stab leading edge, instead of downthrust. As it is, you would have to cut a wedge underneath the stab, bend it down to tilt in some "down" stabilizer, then glue it back It doesn't take much, typically. but does require refinishing.
Brett