Mailing List lml@lancaironline.net Message #14318
From: Marvin Kaye <marv@lancaironline.net>
Subject: Re: [LML] Stall recovery and spin avoidance
Date: Tue, 09 Jul 2002 21:06:38 -0400
To: <lml>


Posted for John Jessen <jjessen@CMBINFO.com>:
Nice post.  Keep it up.  John

-----Original Message-----
Wrom: LKBRNVWWCUFPEGAUTFJMVRESKPNKMBIPBARH

    This is beginning to sound like a discussion about the 'boggy man'.
First consider the loss of lift at the full stall.  Approximately 10% of
the total.   Second consider the loss of Q from a couple of knots above
the stall to stalled.  Less than 2 %   Third consider the stall
progression.  Trailing edge root to tip.  Finally in a Lancair you do
not have all the aileron in the world and you don't have much
deflection.  The ball in your turn coordinator or turn and bank is big,
biggest black indicator on the panel and this is for a reason as applies
to pilots.  Coordinate. This does not mean 'all the aileron in the
world' or only rudder.
...snip...
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