View Single Post
  #3  
Old February 5th 05, 06:27 AM
Larry Dighera
external usenet poster
 
Posts: n/a
Default

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.