X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Thu, 15 Sep 2005 17:28:02 -0400 Message-ID: X-Original-Return-Path: Received: from mta11.adelphia.net ([68.168.78.205] verified) by logan.com (CommuniGate Pro SMTP 5.0c2) with ESMTP id 723116 for lml@lancaironline.net; Thu, 15 Sep 2005 15:46:09 -0400 Received-SPF: pass receiver=logan.com; client-ip=68.168.78.205; envelope-from=dfs155@adelphia.net Received: from f3g6s4 ([67.22.46.165]) by mta11.adelphia.net (InterMail vM.6.01.04.01 201-2131-118-101-20041129) with SMTP id <20050915194525.GGMX27017.mta11.adelphia.net@f3g6s4> for ; Thu, 15 Sep 2005 15:45:25 -0400 X-Original-Message-ID: <002301c5ba2e$b2ed8660$a52e1643@losaca.adelphia.net> From: "Dan Schaefer" X-Original-To: "Lancair list" Subject: Re: airframe vibration X-Original-Date: Thu, 15 Sep 2005 12:50:17 -0700 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 6.00.2800.1437 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1441 FWIW, guys, on my early 235, I had the "grey soot" streaks behind the left outboard elevator hinge early on (at maybe 300 airframe hours). I replaced all the elevator hinge pins with the Teflon sheathed wire at that time and haven't noticed any further wear there over the next 500 hours. As a result, I watched the aileron hinges carefully for development of excessive wear (my criterion: ANY noticeable wear) and replaced those hinge-pins with the same material as the elevator pins at about 400 hours. Same results. Flap hinge-pins have not needed replacement. Having seen high-speed motion pictures of wind tunnel flutter testing - and the catastrophic results of various defects, including loose flight control hinges, among others - I wouldn't fly my LNC2 with even the slightest slop in those hinges. Dan Schaefer