Thanks Larry. I have been reading up on the Skyview sys which I have for my 
panel. I wasn't aware of all the capabilities of the system. You mentioned that 
you had helped install a Skyview sys w/ AoA in a friend's RV-10. I haven't 
completely digested all the features of the Skyview sys. Does the AoA require 
an additional component or is it a built-in feature of the system? If it is 
part of the system, I may just purchase the static/AoA probe and sell the 
Advanced Flight AoA package. Decisions, decisions.
Pete

> Date: Wed, 24 Feb 2016 22:29:00 -0600
> To: pkengr at hotmail.com
> From: flesner at frontier.com
> Subject: RE: KR> Angle of Attack sys
> 
> At 08:35 PM 2/24/2016, you wrote:
> >I misspoke. The unit I have is the Sport not the Pro version where 
> >you have to install pressure ports in the bottom and top of the wing 
> >somewhere between 15 to 40% of the wing chord.
> ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
> 
> Pete,
> 
> Looking at the 125 page document ( 
> http://www.advanced-flight-systems.com/Support/AOAsupport/aoasupport.html 
> ), they seem to imply that it is not that critical as long as you 
> follow the  "don't place near tip, propeller arc, etc., as long as 
> the top and bottom are located at the same % of chord and offset by 2 
> to 4 inches ( I think that's what I read).
> 
> A mid wing location would have a chord of approx 42 inches.  25% 
> would be 10.5 inches and I think that would be just behind the 
> spar.  I'm guessing at these measurements but that's where I think 
> I'd locate them.  A small access panel for installation could be cut 
> BEHIND each port.  Check the site in  blue below.  May be more info there.
> 
> Larry
> 
> 
> =======================
> page 40
> 
> There are some places where pressure ports should
> not be located on the wing such as in line with the
> propeller wash, too close to the wing tip, and in areas
> difficult to access. Generally 15% to 40% chord and
> forward of the ailerons will work well. The upper and
> lower ports should be located at the same % chord but
> offset by 2" to 4" spanwise.
> A. Pick the pressure port locations. For the best wing
> port locations, check the Appendix I or better yet,
> our web site at
> www.angle-of-attack.com
> for the
> most recent information.
> 

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