The CFII further said that,
“All spins are pilot induced.” I
suppose so, as the AOA increased it is likely that right rudder is used
to offset P-factor. If these two forces are not balanced at the stall the
plane probably falls off to one side or the other. Perhaps one of our aerobatic 300
series brethren could comment further (Mark?) as I don’t do stalls or
spins. Having no experience
entering a Lancair spin, upon entering one I would simultaneously pull the
power and momentarily cover my eyes – this would seem to be correct as both
hands would be off the controls for a bit. I guess I should still await comment
from those more experienced (that’s easy, isn’t it?). The real issue with slick Lancairs is
how quick they are at leaving a safe flight regime and then how quick they are
at furthering the depth of any abnormal flight regime.
And other obscure
performance puzzles.
Grayhawk
Only 70 hours more to
safety.