Under what weight conditions is Vmc determined? According to part 23, it says most unfavorable weight--which would be a lesser weight, correct? What specific weight would they use? Please site references. Thanks in advance.
Maximum available power on operating engine.
Critical engine windmilling (or feathered if an auto feather is installed.)
Landin Gear retracted.
Flapsin Takeoff position.
Aft C.G.
Max Gross Weight.
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