Same thing I knew, but if so, it's confusing, how does it come the explanation that VMC changes with bank angle? If there is a difference between wings level and 5 bank towards operative engine, I figure out there is also a difference in turns, right?
For example, if it fails and because of course you don't have an instant reaction, the airplane reaches a bank angle towards the dead engine, let's say 25 degrees, if VMC rises in this case it will reach a value maybe even above blue line, in this case the recovery is to reduce all the power on the operating engine and to hope you haven't already strike the ground. That's why i'm strugling to figure it out, I think there is a great difference if VMC changes with bank angle in a manner that you can't go back to wings level using opposite aileron. Maybe VMC is just for straight and level i.e. you still have aileron to control the roll and when you reach wings level you can maintain straight and level, but they seem to be coupled yaw/roll loss of control, don't know, just very confused about it.
Actually where I don't get it is if below Vmc you still have control to oppose the roll and to level the wings back or assume the 5 degrees bank into the operative and so reaching again the attitude where you can maintain straight flight. This is what confuses me at all.
To be more precise: you fly at VMC, banked 5 degress towards good engine, you can maintain straight and level flight using this banked 5 degrees attitude and also using full rudder. But let's say you bank 5 degrees towards dead engine because you want to turn in that direction, you don't have anymore rudder if hypotethical you want to assume straight flight using that banked attitude toward the dead engine, but you still have the possibility to roll back towards the good engine and there you have again the authority to maintain straight flight, right? Or I'm wrong and since you left the 5 degrees attitude towards good engine you lose all control and can recover only if you reduce the power on the good engine?