Mailing List lml@lancaironline.net Message #36702
From: Craig Berland <cberland@systems3.net>
Sender: <marv@lancaironline.net>
Subject: [LML] Leading edge pitting
Date: Thu, 13 Jul 2006 14:43:40 -0400
To: <lml>
Craig Gainza wrote: Unfortunately, I did not install static wicks from Napa to Sedona.  I installed the wicks in Sedona and have not noticed any additional pitting since installing them. 
My question to the listers: 
    1)  Have any of you experienced similar pitting problems?
    2)  Is the 4-5 foot grounding strap too long? 
    3)  Should the bottom skin be grounded as well?
    4)  Have I adequately dealt with this issue by installing the wicks?
I am heading back to the paint shop on Friday and want to make sure I have resolved this issue.  Any comments are greatly appreciated!
 
Craig, I have found carbon is very conductive but you have to sand down to carbon fibers.  I would check the conductivity of every skin back to a common point.  That is the wing top skin and the wing bottom skin, the horizontal top and the horizontal bottom, the fuselage top and bottom....you get the picture.  I have been told a max of 10 ohms is acceptable.  I would think if each skin is well bonded to all others, 10 ohms would be pretty easy to achieve.  I have seen .03 ohm in a distance of 5 feet.
Craig Berland
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