X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sun, 02 Oct 2011 22:27:03 -0400 Message-ID: X-Original-Return-Path: Received: from raven.ravenwebhosting.com ([72.9.254.67] verified) by logan.com (CommuniGate Pro SMTP 5.4.1) with ESMTPS id 5143078 for lml@lancaironline.net; Sun, 02 Oct 2011 11:04:21 -0400 Received-SPF: none receiver=logan.com; client-ip=72.9.254.67; envelope-from=paul@tbm700.com Received: from s01060017ee00b6c0.cg.shawcable.net ([174.0.115.173]:61207 helo=[192.168.15.6]) by raven.ravenwebhosting.com with esmtpsa (TLSv1:AES128-SHA:128) (Exim 4.69) (envelope-from ) id 1RANZw-0008Fz-Oe for lml@lancaironline.net; Sun, 02 Oct 2011 11:03:45 -0400 Content-Type: text/plain; charset=us-ascii Mime-Version: 1.0 (Apple Message framework v1084) Subject: Re: [LML] Re: Wick mechanical connection From: paul miller In-Reply-To: X-Original-Date: Sun, 2 Oct 2011 09:03:08 -0600 Content-Transfer-Encoding: quoted-printable X-Original-Message-Id: <336C7E9D-B936-41E8-92BF-D0C1FD173737@tbm700.com> References: X-Original-To: "Lancair Mailing List" X-Mailer: Apple Mail (2.1084) X-AntiAbuse: This header was added to track abuse, please include it with any abuse report X-AntiAbuse: Primary Hostname - raven.ravenwebhosting.com X-AntiAbuse: Original Domain - lancaironline.net X-AntiAbuse: Originator/Caller UID/GID - [47 12] / [47 12] X-AntiAbuse: Sender Address Domain - tbm700.com X-Source: X-Source-Args: X-Source-Dir: I second Colyn's comments that non-conducting pieces should be prepared = for static dissipation. There are also many anti-static primers that = can be used then finished with normal aircraft topcoats. An important = requirement if you do the painting yourself is to make the primer = continue from the outside surface around the inside mating surfaces = where it will further conduct to metal or other conductive primer or = conductive composite. The military aircraft shop here in Calgary = explained that the static on the exterior paint will work through the = topcoat layers easily to the primer and then migrate towards the wicks. = If a continuous large circuit is not available, charges build up until a = gap can be jumped (100,000 volts is not unusual for p-static) and then = you'll get unexplained pitting in the paint, pinholes, burn marks, = static in the radios that can render them completely unusable in snow, = and flashes are night that look like BBQ igniters where charges are = jumping gaps. Of course, some climates like Florida don't get the same = reaction in fair weather but up north here where it is dry, the = conditions are magnified. I had to have a new paint job stripped on = all the fibreglass components to solve this issue (wingtips, cowls). I = found in my research that very few of the southern aircraft painters = even knew about this issue so it is important to query the paint shops = on how they will deal with static and how they ensure a continuous path = from forward surfaces back to the wicks. Paul Miller Calgary On 2011-10-02, at 8:08 AM, Colyn Case wrote: > I didn't read this whole thread. Did someone talk about connecting = from the braid that comes from the hstab to the wick connection? My = conclusion was you need a wire from where the braid connects to the = elevator to the wick socket(s) on the back of the elevator. Most of = the static will collect on the leading edge of the hstab, hopefully flow = through the carbon to your amazingly low resistance (1 ohm?) braid = connection, across the braid, through the connection to the wire, = through the wire, into the socket, and out the wick. >=20 > While you're there consider high resistance conductive paint on all = fiberglas surfaces that contain a leading edge. This will allow the = charge to migrate to the back where hopefully you can figure out a way = to get it to a wick. This is the stuff they use on radomes in bigger = airplanes. Here's the info on the paint. As far as I can tell, what = you want is CA7870.