swh,
we are talking about multi engine aircraft here.... single-engine-Vmc in a twin is limited by loss of control due to asymmetric thrust (and not enought rudder force to counteract it), not stalling AOA like in single engine aircarft. (unless you are in a situation where Vmc is below stall speed, like at altitude, but thats another story)
Thanks for contributing though.
palgia
Edited so that it would make sense
