Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Wed, 26 Nov 2003 21:29:49 -0500 Message-ID: X-Original-Return-Path: Received: from hawk.mail.pas.earthlink.net ([207.217.120.22] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2774250 for lml@lancaironline.net; Wed, 26 Nov 2003 20:13:04 -0500 Received: from sdn-ap-002watacop0095.dialsprint.net ([63.187.200.95] helo=f3g6s4) by hawk.mail.pas.earthlink.net with smtp (Exim 3.33 #1) id 1APAiN-00050D-00 for lml@lancaironline.net; Wed, 26 Nov 2003 17:13:04 -0800 X-Original-Message-ID: <006301c3b484$2d377dc0$5fc8bb3f@f3g6s4> Reply-To: "Dan Schaefer" From: "Dan Schaefer" X-Original-To: "Lancair list" Subject: Re: Help wanted with rudder/aileron trim tabs X-Original-Date: Wed, 26 Nov 2003 17:17:07 -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 6.00.2800.1158 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 Bill, I agree with Ray Gardner regarding a rudder trim tab. IMHO, it isn't needed. An Aileron tab, however, is useful - at least I've found it so particularly when I go from flying solo to squeezing a 200lb passenger into the right seat. The aircraft's response to that much change in lateral loading makes a roll trim very nice to have. Mine is a hinged aluminum strip about 1 inch x 6 inches on the inboard end of the right aileron and it's effectiveness is way more than adequate - Takes very little tab deflection to trim for straight and level with any of the lateral unbalances I've ever flown with (admittedly, I haven't explored the extremes but am satisfied with my trim power for conditions I consider nominal - beyond which I wouldn't fly, anyway). Dan Schaefer Early LNC2