Vmcg turning moment
Wouldn't that apply to the turning moment of the remaining engine(s) as well?
Less abrupt yaw, - better rudder control, if you (read me!) are a little slow applying rudder?
Basically, I would think, the yaw moment (force X arm), with assymetric thrust is not dependent upon CG, and the yaw moment of the rudder would only be dependent upon deflection and speed? Aft CG would only result in a slower yaw (tail sideways) acceleration?
Wow, this was complicated, and it's getting worse!