During the public discussion on this issue, one pilot wrote
in a in a letter to the editor (might have been in AWST)
that as far back as the DC-3 pilots had been aware that you
couldn't just throw in full rudder deflection on an
airliner as if it were a Gypsy Moth. The stabilizer/rudder is
an airfoil, and it will break when subjected to a certain force.
This force in turn is a function of several parameters, most
importantly dynamic pressure or indicated airspeed, yaw angle,
and lift coefficient (determined by the rudder angle; I have
heard that full rudder deflection increases the lift coefficient
by about 50 percent). How difficult would it be to set up a
simulator with accurate information about the behaviour of an
airliner at extreme yaw angles so as to teach pilots to
recognize and avoid situations where they are verging on
stabilizer failure?
Thank you,
Peter Wezeman
anti-social Darwinist
"Forty gallons; not enough to measure, really."