X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from omr-m09.mx.aol.com ([64.12.143.82] verified) by logan.com (CommuniGate Pro SMTP 6.0.8) with ESMTPS id 6725251 for lml@lancaironline.net; Sun, 09 Feb 2014 17:11:31 -0500 Received-SPF: pass receiver=logan.com; client-ip=64.12.143.82; envelope-from=Sky2high@aol.com Received: from mtaomg-mcc01.mx.aol.com (mtaomg-mcc01.mx.aol.com [172.26.253.85]) by omr-m09.mx.aol.com (Outbound Mail Relay) with ESMTP id 659BE701CBF63 for ; Sun, 9 Feb 2014 17:10:56 -0500 (EST) Received: from core-mlc005c.r1000.mail.aol.com (core-mlc005.r1000.mail.aol.com [172.29.188.211]) by mtaomg-mcc01.mx.aol.com (OMAG/Core Interface) with ESMTP id 3F56438000082 for ; Sun, 9 Feb 2014 17:10:56 -0500 (EST) From: Sky2high@aol.com Full-name: Sky2high Message-ID: Date: Sun, 9 Feb 2014 17:10:56 -0500 (EST) Subject: Re: [LML] LNCE - Aileron servo wiring To: lml@lancaironline.net MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="part1_b218c.60111a2a.402956f0_boundary" X-Mailer: AOL 9.6 sub 168 X-Originating-IP: [67.175.156.123] x-aol-global-disposition: G DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=mx.aol.com; s=20121107; t=1391983856; bh=oiJHN6aXyW+QuSOcFTphnMXxz1hW1YIfL0C88VXNzB8=; h=From:To:Subject:Message-ID:Date:MIME-Version:Content-Type; b=Zl9rAm0yVnkxIb/6w4sCuluUa5QTQ3BPhGVrmwLmi7a/2Y9Yoyv3dC03R8FdeDkwz kgp6PymfClv/mJS1kFNrX7kuxkegKEmsM6yirpBKpQWIa6l+RLMV1cb92vFAs3lWFf tLqkF5IotwWGOSIG4xPX68fx8VWxZ/rKaE++AZlE= x-aol-sid: 3039ac1afd5552f7fcf00df6 --part1_b218c.60111a2a.402956f0_boundary Content-Type: text/plain; charset="UTF-8" Content-Transfer-Encoding: quoted-printable Content-Language: en Jim, =20 Another way is to exit the fuselage at a point and enter the aileron at a= =20 point that is say, 6 inches either inboard or outboard of the other point.= =20 This allows the flex (twist) to occur along the 6 inches rather that=20 actually have a single bend point. Encasing the whole run in flexible tub= ing=20 (Tygon?) is useful to protect the wires from chafing and the weather. =20 Grayhawk =20 =20 In a message dated 2/9/2014 3:26:44 P.M. Central Standard Time, =20 snopercod@comporium.net writes: Jim-- The way you described is exactly how I did it on my L-235. --John On 2/8/2014 6:00 AM, Lancair Mailing List wrote: Subject: =20 LNCE - Aileron servo wiring =20 From: =20 "James M. Anderson, III P.C." __=20 (mailto:jma@jmalawfirm.com) =20 Date: =20 2/7/2014 8:26 AM =20 To:=20 _lml@lancaironline.net_ (mailto:lml@lancaironline.net)=20 =20 =20 Greetings! Things are going pretty well with my ES, but shockingly I have= =20 a question that is not really answered by the manual or any other source. = =20 I need to run wiring from the aileron servo to the wing tip, eventually=20 proceeding through the leading edge conduit. I=E2=80=99ve bonded in a len= gth of =C2=BC=20 inch nylon tubing along the forward edge of the aileron spar for this=20 purpose. My question is where to exit from the aileron? I=E2=80=99m thi= nking that the=20 place with the least amount of bending during operation is right at the=20 hinge line (as suggested in the manual), leaving holes both in the aileron= =20 close-out and the wing tip rib. Is there a better way to do this? --part1_b218c.60111a2a.402956f0_boundary Content-Type: text/html; charset="UTF-8" Content-Transfer-Encoding: quoted-printable Content-Language: en
Jim,
 
Another way is to exit the fuselage at a point and enter the aile= ron=20 at a point that is say, 6 inches either inboard or outboard of the other=20 point.  This allows the flex (twist) to occur along the 6 inches= =20 rather that actually have a single bend point.  Encasing the whol= e=20 run in flexible tubing (Tygon?) is useful to protect the wires from ch= afing=20 and the weather.
 
Grayhawk
 
In a message dated 2/9/2014 3:26:44 P.M. Central Standard Time,=20 snopercod@comporium.net writes:
=
Jim--

The way you described is exactl= y how I=20 did it on my L-235.

--John

On 2/8/2014 6:00 AM, Lancair Mai= ling=20 List wrote:
Subject:= =20
LNCE - Aileron servo wiring
From:=20
"James M. Anderson, III P.C." <jma@jmalawfirm.com>=
Date:=20
2/7/2014 8:26 AM
To: lml@lancaironline.net

Greetings!  Things are going pretty well with= my ES,=20 but shockingly I have a question that is not really answered by the man= ual=20 or any other source.  I need to run wiring from the aileron servo = to=20 the wing tip, eventually proceeding through the leading edge conduit.&n= bsp;=20 I=E2=80=99ve bonded in a length of =C2=BC inch nylon tubing along the f= orward edge of the=20 aileron spar for this purpose.  My question is where to exit from = the=20 aileron?   I=E2=80=99m thinking that the place with the least= amount of=20 bending during operation is right at the hinge line (as suggested in th= e=20 manual), leaving holes both in the aileron close-out and the wing tip= =20 rib.  Is there a better way to do=20 this?


--part1_b218c.60111a2a.402956f0_boundary--