Larry,

Sorry for the confusion on the BRS installer....

Do you know if there was any design justification or reasons for the KR2's
inability of recovery from a spin? Was it because of the designer wanted to
make the bird a bit lighter by restricting the rudder/aileron control
surfaces a bit too stringent needed for recovering should someone get into
a spin by human errors, perhaps?!

Thanks,

Dr. Hsu

On Tue, Apr 13, 2021, 7:02 AM Flesner <fles...@frontier.com> wrote:

> On 4/13/2021 7:43 AM, shafferj45...@twc.com wrote:
> > Just before the
> > break, it would shudder, shake, practically screaming to tell you it
> > was about to stall. I always figured this was due to the 3 degrees of
> > washout built into the wing.
>
> +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
>
> The 3 degree washout in the wing causes the wing root to stall first and
> keeps the air attached over the area of the ailerons to help maintain
> roll control.  It is quite effective as I observed when I "tuffed" the
> right wing and did stalls. I have video but not tech knowledgeable
> enough to load to Youtube.  In a straight ahead level stall, as in the
> flare, the air stays attached to the outer wing and I have roll control
> without use of the rudder.  In that type of stall the chance of a spin
> is remote.  Anyone doing spins in an untested airplane without a drag
> chute for recovery is strictly on their own.
>
> Larry Flesner
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