Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Sat, 13 Mar 2004 01:03:48 -0500 Message-ID: X-Original-Return-Path: Received: from albatross.mail.pas.earthlink.net ([207.217.120.120] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 3076798 for lml@lancaironline.net; Sat, 13 Mar 2004 00:00:44 -0500 Received: from 0-1pool119-142.nas8.tucson1.az.us.da.qwest.net ([67.0.119.142] helo=Downstairs) by albatross.mail.pas.earthlink.net with smtp (Exim 3.33 #1) id 1B21GN-00064g-00 for lml@lancaironline.net; Fri, 12 Mar 2004 21:00:44 -0800 X-Original-Message-ID: <000701c408c0$803c6040$0100a8c0@Downstairs> From: "Robert Smiley" X-Original-To: "Lancair Mailing List" References: Subject: Re: [LML] Re: LNC4 T AC and rudder question X-Original-Date: Fri, 12 Mar 2004 22:00:33 -0800 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1158 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 Install on the rudder pedals where the tension springs are located a carriage bolt with the round portion of the head ground off, drill a hole in the rectangular portion of the head to insert the spring ends and fabricate a mount for the other end and use a wing nut for variable tension adjustment. I used different springs than those provided in the plane kit. The objective is to use the lightest tension possible but accomplish the effect to impart a differential load on the system. Does not take much to do so. You load one side more than the other by tightening up one and lossening the other wing nut. Bob Smiley