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Originally Posted by tgrayson  Supposedly, it the maximum encountered crosswind during flight testing. I'm skeptical that this is the entire story, though. Seems a little coincidental that the maximum wind encountered during testing is so close among aircraft of the same market segment. My suspicion is that the flight testers seek out particular wind velocities that are sufficient for marketing purposes and have little motivation to put the airplane to its limits.
BTW, Part 23 only requires a capability of .2Vs0.
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Where's the picture from? Maybe a before and after picture would help, as in ball centered and no bank first, ball towards the good engine and banked second?
Is it safe to say that you're essentially slipping back into the good engine when you "raise the dead?" I'm still having trouble seeing why with the ball centered there is a net force (yet no yaw?) moving the entire aircraft in the direction of the bad engine. Is the force solely the result of rudder input to counteract the yaw from the good engine?