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<DIV><FONT face=Arial size=2>The lead wing is seeing a rapidly increasing angle
of attack due to elevator input. When the aileron initiates this exceeds
the stall angle of attack for the lead wing. The lagging wing is seeing a
reduced angle of attack and does not stall.</FONT></DIV>
<DIV><FONT face=Arial size=2></FONT> </DIV>
<DIV><FONT face=Arial size=2>Stall is independent of speed and dependent on
angle of attack.</FONT></DIV>
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<DIV><FONT face=Arial size=2>Inputs for all three axis can be initiated
simultaneously.</FONT></DIV></BODY></HTML>