deadringer86
Well-Known Member
Quick question here that has me stumped. We know that a heavier airplane has a lower Vmc since it can generate a greater horizontal component of lift at a given bank angle than a lighter aircraft. Therefore, we need less bank to counteract the sideslip. However, there is also the rule of thumb that Vmc decreases 3 knots per 1 degree of bank into the operating engine. Ignoring aircraft performance, wouldn't this contradict the weight theory as far as actual Vmc speed?