Centaurus
Consider the case where you are doing a straight pull out close to or at the limiting g for the aircraft. That specified limiting g will have a margin of structural strength for safety. Then you apply aileron to roll. Immediately you begin to overload the wing with the extra lift produced by the down going aileron. In extreme cases the up going wing will overload to the structural limit and fail.
It's called a rolling pull out. Beware and avoid like the plague..