"Larry Dighera" wrote in message
...
On Fri, 4 Feb 2005 19:14:09 -0600, "John W. Galvin"
wrote in
::

The Cirrus is supposedly recoverable in a spin, with one change
from the usual procedu the yoke is supposed to be
moved briskly forward to the stop.

That's interesting. First I've heard of it. What is the source of
that information?

I presume that spin recovery method is not mentioned in the POH. I
can imagine situations where it might be preferable to 'chute
deployment if it was truly a certifiable spin recovery option.

Your e-mail address looked valid. I don't want to know how much spam you
must receive. I sent you a copy of the JAA PDF. It documents the method
mentioned.

The POH for the SR22 had spin recovery documented, but that text was removed
in later revisions in favor of the CAPS as only method of spin recovery. My
guess would be that the lawyers made that decision.

--Galvin