X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Fri, 07 Feb 2014 08:26:02 -0500 Message-ID: X-Original-Return-Path: Received: from mailout18.yourhostingaccount.com ([65.254.253.149] verified) by logan.com (CommuniGate Pro SMTP 6.0.8) with ESMTP id 6721491 for lml@lancaironline.net; Thu, 06 Feb 2014 14:39:47 -0500 Received-SPF: pass receiver=logan.com; client-ip=65.254.253.149; envelope-from=SRS0=A1hLk2=XL=jmalawfirm.com=jma@yourhostingaccount.com Received: from mailscan21.yourhostingaccount.com ([10.1.15.21] helo=mailscan21.yourhostingaccount.com) by mailout18.yourhostingaccount.com with esmtp (Exim) id 1WBUn0-0004ux-PF for lml@lancaironline.net; Thu, 06 Feb 2014 14:39:11 -0500 Received: from impout02.yourhostingaccount.com ([10.1.55.2] helo=impout02.yourhostingaccount.com) by mailscan21.yourhostingaccount.com with esmtp (Exim) id 1WBUn0-0002EK-Fo for lml@lancaironline.net; Thu, 06 Feb 2014 14:39:10 -0500 Received: from authsmtp12.yourhostingaccount.com ([10.1.18.12]) by impout02.yourhostingaccount.com with NO UCE id P7fA1n0020FdXoS017fAUs; Thu, 06 Feb 2014 14:39:10 -0500 X-Authority-Analysis: v=2.0 cv=Y4J6Q2iN c=1 sm=1 a=REvN6aXKysu9SPD4Wa7Dfw==:17 a=7lQ0IRkrd_EA:10 a=1UaXI4RFVuMA:10 a=jCjMekOTAAAA:8 a=T-5UpORNk6MA:10 a=8A7brI4kjU8C6ETGAX3PRdgeao0=:19 a=JVLz3kuRcOGypWGGtvgA:9 a=wPNLvfGTeEIA:10 a=VAl9GSzx4W4A:10 a=v2sp6JMV-C8A:10 a=qkNJV05DaXWauZFj:21 a=xYi3ckbghQVrO0Do:21 a=yMhMjlubAAAA:8 a=SSmOFEACAAAA:8 a=8GUrmZcixkblmZ4yzJEA:9 a=gKO2Hq4RSVkA:10 a=UiCQ7L4-1S4A:10 a=hTZeC7Yk6K0A:10 a=frz4AuCg-hUA:10 a=aL17PzI6kw2fkSsK:21 a=gWrbnHpLD-gStEu5:21 a=t1ijpx9AV50gTBtUFlM2vg==:117 X-EN-OrigOutIP: 10.1.18.12 X-EN-IMPSID: P7fA1n0020FdXoS017fAUs Received: from 99-46-188-39.lightspeed.tukrga.sbcglobal.net ([99.46.188.39]:55662 helo=JIM02) by authsmtp12.yourhostingaccount.com with esmtpa (Exim) id 1WBUn0-0004rC-2G for lml@lancaironline.net; Thu, 06 Feb 2014 14:39:10 -0500 From: "James M. Anderson, III P.C." X-Original-To: "Lancair Mailing List" Subject: LNCE - Aileron servo wiring X-Original-Date: Thu, 6 Feb 2014 14:39:22 -0500 X-Original-Message-ID: <005401cf2373$239ac330$6ad04990$@com> MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0055_01CF2349.3AC4BB30" X-Mailer: Microsoft Office Outlook 12.0 Thread-Index: Ac8jcyKQ0Qq6qLZySGupbYwm+h/qbg== Content-Language: en-us X-EN-UserInfo: 30bd57614b4f7ec2f519431e7812f4ff:931c98230c6409dcc37fa7e93b490c27 X-EN-AuthUser: jma@jmalawfirm.com X-Original-Sender: "James M. Anderson, III P.C." X-EN-OrigIP: 99.46.188.39 X-EN-OrigHost: 99-46-188-39.lightspeed.tukrga.sbcglobal.net This is a multi-part message in MIME format. ------=_NextPart_000_0055_01CF2349.3AC4BB30 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Greetings! Things are going pretty well with my ES, but shockingly I = have a question that is not really answered by the manual or any other source. = I need to run wiring from the aileron servo to the wing tip, eventually proceeding through the leading edge conduit. I=92ve bonded in a length = of =BC inch nylon tubing along the forward edge of the aileron spar for this purpose. My question is where to exit from the aileron? I=92m = thinking that the place with the least amount of bending during operation is right at = the hinge line (as suggested in the manual), leaving holes both in the = aileron close-out and the wing tip rib. Is there a better way to do this? =20 =20 By the way, is the whole country laughing at Atlanta=92s clearly inept handling of two measly inches of snow? =20 =20 =20 James M. Anderson, III Anderson & Ealick, P.C. Suite 130 5855 Sandy Springs Circle Sandy Springs, GA 30328 404-255-0319 jma@jmalawfirm.com =20 ------=_NextPart_000_0055_01CF2349.3AC4BB30 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable

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

 

By the way, = is the whole country laughing at Atlanta’s clearly inept handling = of two measly inches of snow? 

 

 

James = M. Anderson, III

Anderson & Ealick, P.C.

Suite 130

5855 Sandy Springs = Circle

Sandy = Springs,=A0 GA=A0 30328

404-255-0319

jma@jmalawfirm.com

 

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