Return-Path: Sender: (Marvin Kaye) To: lml Date: Tue, 19 Nov 2002 14:20:02 -0500 Message-ID: X-Original-Return-Path: Received: from pop3.olsusa.com ([65.115.173.155] verified) by logan.com (CommuniGate Pro SMTP 4.0.1) with ESMTP id 1882076 for lml@lancaironline.net; Tue, 19 Nov 2002 14:13:51 -0500 Received: from swan.mail.pas.earthlink.net ([207.217.120.123]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71866U8000L800S0V35) with ESMTP id com for ; Tue, 19 Nov 2002 14:03:54 -0500 Received: from sdn-ap-007watacop0006.dialsprint.net ([65.176.64.6] helo=f3g6s4) by swan.mail.pas.earthlink.net with smtp (Exim 3.33 #1) id 18EDoj-0007Lo-00 for lancair.list@olsusa.com; Tue, 19 Nov 2002 11:13:50 -0800 X-Original-Message-ID: <004401c28fff$c5e2c200$0640b041@f3g6s4> Reply-To: "Dan Schaefer" From: "Dan Schaefer" X-Original-To: "Lancair list" Subject: Re: Navaid Autopilot (afterthought) X-Original-Date: Tue, 19 Nov 2002 11:13:39 -0800 MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1106 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 In response to D. Story's post, your surmise that there is no way to connect the servo actuator to the aileron push-rod is incorrect as that is exactly how I installed mine. The servo output push-rod is connected directly to the intermediate lever in the stub wing where the inboard and outboard push rods are connected. (at the push-rod disconnect for wing removal). The servo is mounted beneath the passenger seat, just behind the stick mechanism with the output shaft facing forward. I had a shaft extension facricated that fits onto the servo shaft and is pinned with a roll pin. The extension (about 4 - 5 inches long) is supported at the forward end by a bearing and pin that is mounted on the aft face of the spar shear web. An output lever, the same size as the servo putput lever (which is not used), is welded to the extension at the point, an inch or so aft of the support bearing, to allow the actuator push-rod to run directly below and parallel to the main aileron push-rod, thru the close-out rib, to the intermediate lever. With this set-up, there is no pitch input from the autopilot that I can discern. Regards, Dan Schaefer