Return-Path: Sender: (Marvin Kaye) To: lml Date: Thu, 28 Nov 2002 22:32:55 -0500 Message-ID: X-Original-Return-Path: Received: from mailnw.centurytel.net ([209.206.160.237] verified) by logan.com (CommuniGate Pro SMTP 4.0.2) with ESMTP id 1890893 for lml@lancaironline.net; Thu, 28 Nov 2002 22:30:38 -0500 Received: from c656256a (pppoe0623.gh.centurytel.net [209.206.248.152]) by mailnw.centurytel.net (8.12.6/8.12.6) with SMTP id gAT3Ua78012637 for ; Thu, 28 Nov 2002 19:30:37 -0800 (PST) X-Original-Message-ID: <000901c29750$03e4cf60$0100a8c0@mshome.net> From: "Robert Smiley" X-Original-To: "Lancair Mailing List" References: Subject: Re: [LML] Re: Body Work X-Original-Date: Thu, 28 Nov 2002 19:35:42 -0700 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 5.50.4133.2400 X-MimeOLE: Produced By Microsoft MimeOLE V5.50.4133.2400 Dan, Thanks for the ideas. The spider cracks were on the non core top cowling. I did leave the old cracked structure in the system. That was my mistake. Looks like from your instructions that you back up the affected area with preferably two ply diagonally oriented carbon fiber, grind out the old structure to eliminate the cracked areas and build up the affected area with multiple plys of carbon fiber, multiple orientations then finish out with hard epoxies. Thanks Dan. I may do that in the future when it comes time to retouching up the plane. I found out the other day on a bid to repave a mobile home park that they do the same thing. ie remove old cracked pavement and redo it because the older cracked pavement just cracks overlayment over time even though they apply a carbon fiber material in between layers. Bob Smiley