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Date: Sat, 24 Jul 2010 23:10:07 -0400
Subject: re: SPAM-LOW:  [FlyRotary] Re: Tie Down Hardpoints
From: "Thomas Mann" <tmann@n200lz.com>
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To: <flyrotary@lancaironline.net>
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I ended up going with aluminum. =0D=0AThe plate was fabricated from 1/4" Al=
uminum.=0D=0AThe bushing is threaded at 1/2" - 13.=0D=0A=0D=0AThe weight tu=
rned in at 5.1 oz. each.=0D=0A=0D=0A---------------------------------------=
-=0D=0A=0D=0AFrom: "Al Gietzen" <ALVentures@cox.net>=0D=0ASent: Saturday, J=
uly 24, 2010 8:23 PM=0D=0ATo: "Rotary motors in aircraft" <flyrotary@lancai=
ronline.net>=0D=0ASubject: SPAM-LOW: [FlyRotary] Re: Tie Down Hardpoints =
=0D=0A=0D=0AI know, an old thread, but; yes, the oxide layer that forms inh=
ibits further=0D=0Acorrosion of the SS; but imbedding in epoxy (fiberglass)=
 protects it even=0D=0Abetter.=0D=0A=0D=0AAl=0D=0A

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I ended up going with aluminum. <br>The plate was fabricated from 1/4" Alum=
inum.<br>The bushing is threaded at 1/2" - 13.<br><br>The weight turned in =
at 5.1 oz. each.<br><br><font face=3D"Tahoma, Arial, Sans-Serif" size=3D2>=
=0D=0A<hr align=3Dcenter width=3D"100%" SIZE=3D2>=0D=0A<b>From</b>: "Al Gie=
tzen" &lt;ALVentures@cox.net&gt;<br><b>Sent</b>: Saturday, July 24, 2010 8:=
23 PM<br><b>To</b>: "Rotary motors in aircraft" &lt;flyrotary@lancaironline=
.net&gt;<br><b>Subject</b>: SPAM-LOW: [FlyRotary] Re: Tie Down Hardpoints</=
font><br><br>I know, an old thread, but; yes, the oxide layer that forms in=
hibits further<br>corrosion of the SS; but imbedding in epoxy (fiberglass) =
protects it even<br>better.<br><br>Al<br>

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