X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Fri, 09 Mar 2012 11:06:55 -0500 Message-ID: X-Original-Return-Path: Received: from cdptpa-omtalb.mail.rr.com ([75.180.132.120] verified) by logan.com (CommuniGate Pro SMTP 5.4.4) with ESMTP id 5434034 for lml@lancaironline.net; Thu, 08 Mar 2012 14:51:24 -0500 Received-SPF: pass receiver=logan.com; client-ip=75.180.132.120; envelope-from=dfs155@roadrunner.com X-Original-Return-Path: X-Authority-Analysis: v=2.0 cv=TvJkdUrh c=1 sm=0 a=h8T1bDYXFMVBv/yMROfBWA==:17 a=rmUd7mVkTh4A:10 a=fy7onhTEVoEA:10 a=zTVDa7HKqxcA:10 a=8nJEP1OIZ-IA:10 a=PZviidz5Zq9xnvSKwhsA:9 a=N9g770LEcZa3WJ4asRYA:7 a=wPNLvfGTeEIA:10 a=h8T1bDYXFMVBv/yMROfBWA==:117 X-Cloudmark-Score: 0 X-Originating-IP: 98.145.90.66 Received: from [98.145.90.66] ([98.145.90.66:3604] helo=dan) by cdptpa-oedge01.mail.rr.com (envelope-from ) (ecelerity 2.2.3.46 r()) with ESMTP id 51/CB-17039-89D095F4; Thu, 08 Mar 2012 19:50:48 +0000 X-Original-Message-ID: <53B3514718BC409080C81F07520BAB9F@dan> From: "Dan Schaefer" X-Original-To: "Lancair list" Subject: RE:LNC2 - Harmonization between pitch and roll X-Original-Date: Thu, 8 Mar 2012 11:50:42 -0800 MIME-Version: 1.0 Content-Type: text/plain; format=flowed; charset="iso-8859-1"; reply-type=original Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.5931 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.6157 Haven't posted for some time but figured I'd weigh in on this thread. I'm still flying my early LNC-2 (235, first flight in '93) and have over 1100 hours on it (Should have a lot more but there was a lot of down time over the years - not airplane related). I have the early aluminum elevator lever (horn?) and the bob-weight. I found the pitch response adequate but thought the amount of stick displacement for various flight regimes, particularly landing, was excessive. Some time after (or maybe during - hard to remember) the test flight phase, I followed the recommendations of the factory to move the push-rod attach up one inch from what was called out in the build manual. That gave me what I wanted for stick displacement but hardly noticed a change in pitch responsiveness ("sensitivity"?) - most likely due to the bob-weight. As far as I'm concerned, the airplane is a joy to fly though it took a while to become attuned to stick forces required to fly smoothly - particularly when moving from a C-182 or similar spam-can. It did take a bit of trial and error to get the bob-weight adjusted to my liking but haven't changed a thing since then as I really like the "finger-tip" control. Add to that the fact that the only other person to fly the airplane besides myself is an ex-carrier pilot friend (who incidentally flies a Falco) thinks the airplane handles "very nice". Incidentally, my LNC-2's roll-rate will take your hat off if you put the stick hard over but for normal cruising it just requires finger pressure - so what's not to like? Admittedly, pitch sensitivity is somewhat higher than roll but it's quite easy to get used to it. I wouldn't change a thing! Dan Schaefer LNC-2 N235SP