Maybe I should`ve posted the question as Vmc vs Load factor. We seem to have digressed to a discussion of Vmca vs Vmcg which has introduced the novel idea of bank angle effecting Vmcg in special cases. I was hoping JF would contribute and am wondering what he has in mind. Can you have nozzle failures producing the vectored thrust equivalents of minimum control speeds ?. Also a specific q to someone who would display or test a conventional multi engined aircraft how does load factor effect minimum control speed ?.--if indeed it does.