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<p class=MsoNormal><font size=2 color=navy face=Arial><span style='font-size:
10.0pt;font-family:Arial;color:navy'>Thanks Rick! Just what I was looking for.<o:p></o:p></span></font></p>

<p class=MsoNormal><font size=2 color=navy face=Arial><span style='font-size:
10.0pt;font-family:Arial;color:navy'><o:p>&nbsp;</o:p></span></font></p>

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<p class=MsoNormal><b><font size=2 face=Tahoma><span style='font-size:10.0pt;
font-family:Tahoma;font-weight:bold'>From:</span></font></b><font size=2
face=Tahoma><span style='font-size:10.0pt;font-family:Tahoma'>
nsrca-discussion-bounces@lists.nsrca.org [mailto:nsrca-discussion-bounces@lists.nsrca.org]
<b><span style='font-weight:bold'>On Behalf Of </span></b>Rick Wallace<br>
<b><span style='font-weight:bold'>Sent:</span></b> Tuesday, July 25, 2006 12:58
PM<br>
<b><span style='font-weight:bold'>To:</span></b> <st1:PersonName w:st="on">nsrca-discussion@lists.nsrca.org</st1:PersonName><br>
<b><span style='font-weight:bold'>Subject:</span></b> Re: [NSRCA-discussion]
Formula for figuring wing loading?</span></font><o:p></o:p></p>

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<p class=MsoNormal><font size=3 face="Times New Roman"><span style='font-size:
12.0pt'><o:p>&nbsp;</o:p></span></font></p>

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<p><font size=3 face="Times New Roman"><span style='font-size:12.0pt'>Here's an
excel spread sheet that should work for you. <o:p></o:p></span></font></p>

<p><font size=3 face="Times New Roman"><span style='font-size:12.0pt'>Enter
stuff in the yellow boxes: <br>
wing area in sq in<br>
model weight in lb and ounces <o:p></o:p></span></font></p>

<p><font size=3 face="Times New Roman"><span style='font-size:12.0pt'>wing
loading will calculate in the green boxes. <o:p></o:p></span></font></p>

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face=Tahoma><span style='font-size:8.5pt;font-family:Tahoma'>

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<p class=MsoNormal style='margin-bottom:12.0pt'><font size=1 face=Tahoma><span
style='font-size:8.5pt;font-family:Tahoma'>From: <i><span style='font-style:
italic'>&quot;twtaylor&quot; &lt;twtaylor@ftc-i.net&gt;</span></i><br>
Reply-To: <i><span style='font-style:italic'>NSRCA Mailing List &lt;<st1:PersonName
w:st="on">nsrca-discussion@lists.nsrca.org</st1:PersonName>&gt;</span></i><br>
To: <i><span style='font-style:italic'>&lt;<st1:PersonName w:st="on">nsrca-discussion@lists.nsrca.org</st1:PersonName>&gt;</span></i><br>
Subject: <i><span style='font-style:italic'>[NSRCA-discussion] Formula for
figuring wing loading?</span></i><br>
Date: <i><span style='font-style:italic'>Tue, 25 Jul 2006 10:36:20 -0400</span></i><o:p></o:p></span></font></p>

<blockquote style='border:none;border-left:solid #A0C6E5 1.5pt;padding:0in 0in 0in 4.0pt;
margin-left:3.75pt;margin-top:5.0pt;margin-right:0in;margin-bottom:5.0pt'>

<p class=MsoNormal><font size=2 face=Arial><span style='font-size:10.0pt;
font-family:Arial'>For the mathematically impaired (me) Anyone know the
formula?&nbsp; I&#18;d like to plug and play some numbers. Thanks</span></font><o:p></o:p></p>

<p class=MsoNormal><font size=1 face=Tahoma><span style='font-size:8.5pt;
font-family:Tahoma'><o:p>&nbsp;</o:p></span></font></p>

<p><font size=1 face=Tahoma><span style='font-size:8.5pt;font-family:Tahoma'>&gt;_______________________________________________<br>
&gt;NSRCA-discussion mailing list<br>
&gt;NSRCA-discussion@lists.nsrca.org<br>
&gt;http://lists.nsrca.org/mailman/listinfo/nsrca-discussion<o:p></o:p></span></font></p>

</blockquote>

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