Return-Path: Received: from baron.nii.net ([209.113.172.16]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Sat, 3 Jun 2000 10:56:42 -0400 Received: from nii.net (xcom9.nii.net [209.113.173.73]) by baron.nii.net (8.9.3/8.9.3) with ESMTP id LAA02728 for ; Sat, 3 Jun 2000 11:02:43 -0400 Message-ID: <39391E11.59797A3A@nii.net> Date: Sat, 03 Jun 2000 11:02:41 -0400 From: "Angier M. Ames" Reply-To: alphadog@nii.net Organization: Alpha Delta Research To: lancair.list@olsusa.com Subject: Re: LNC2 Aileron tab References: <20000603050056.AAA1794@ns1.olsusa.com> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I'm about to balance my left aileron but before I do, I need to determine the best way to route and secure the 2 conductor wire for the Mac servo which controls the tab. I want to eliminate any vibration or chafing for these wires in a way that does not complicate the aileron install process and also need to decide on the best location for the connector. Early on in wing constrtuction, I ran the trim tab wiring out to the tip and aft toward the tip TE. It penetrates the tip closeout rib just behind the wing rear spar and I was planning to run the wire into the aileron and make the connection inside the aileron. Now I'm thinking this may not be the best idea. It would seem better to make a permanent connection in the aileron, secure the wire along the forward face of the aileron spar, run the wire into the wingtip and make the connection inside the wingtip. I did build an access panel into each wingtip. I'm hoping that some of you could describe your solution/s to this problem. Thanks, Angier Ames >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>