Originally Posted by NickLappos
<<trim & snip>>
...where the lateral cyclic trim (where the cyclic needs to be to keep the wings level) begins to move rapidly toward the retreating side. Eventually, the cyclic hits the stops and the aircraft rolls toward the advancing side. At the same time, the nose tries to lift, so the cyclic needs to go somewhat forward.
Nick, am I way off base, or did you reverse the bolded bits?
