X-Virus-Scanned: clean according to Sophos on Logan.com X-SpamCatcher-Score: 1 [X] Return-Path: Sender: To: lml Date: Thu, 08 Feb 2007 11:05:20 -0500 Message-ID: X-Original-Return-Path: Received: from elasmtp-dupuy.atl.sa.earthlink.net ([209.86.89.62] verified) by logan.com (CommuniGate Pro SMTP 5.1.6) with ESMTP id 1824046 for lml@lancaironline.net; Thu, 08 Feb 2007 10:27:44 -0500 Received-SPF: none receiver=logan.com; client-ip=209.86.89.62; envelope-from=rtitsworth@mindspring.com DomainKey-Signature: a=rsa-sha1; q=dns; c=nofws; s=dk20050327; d=mindspring.com; b=rY85jOnMzHFsoQ+cWe3KkaJdaK0x3YHeaNZs446A8P45K/fPqMmmV5nC1wV64FNK; h=Received:From:To:Subject:Date:Message-ID:MIME-Version:Content-Type:Content-Transfer-Encoding:X-Mailer:Thread-Index:In-Reply-To:X-MimeOLE:X-ELNK-Trace:X-Originating-IP; Received: from [68.40.94.44] (helo=RDTVAIO) by elasmtp-dupuy.atl.sa.earthlink.net with asmtp (Exim 4.34) id 1HFAzr-0005mO-5o for lml@lancaironline.net; Thu, 08 Feb 2007 10:15:39 -0500 From: "rtitsworth" X-Original-To: "'Lancair Mailing List'" Subject: Wing Skin Fix Question X-Original-Date: Thu, 8 Feb 2007 10:15:21 -0500 X-Original-Message-ID: <008e01c74b93$f3abd970$6400a8c0@RDTVAIO> MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit X-Mailer: Microsoft Office Outlook 11 Thread-Index: AcdLUYF5R8lnWzewTzWK668yZkugXgAQMgyg In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.3028 X-ELNK-Trace: b17f11247b2ac8f0a79dc4b33984cbaa0a9da525759e265402a6a587cb213525880a944458d5573d8f1403e8a44865d0350badd9bab72f9c350badd9bab72f9c X-Originating-IP: 68.40.94.44 FYI, Does anyone have any experience/suggestions on how you would fix a serious Ding in an upper wing skin. By "Ding" I mean a 3" hole/crack all the way through the skin (outer/core/inner). Assume the hole/crack is over the fuel bay and inaccessible from the inside/bottom. I'm thinking that either: A): The entire skin needs to be removed to fix the inside and re-apply fuel sealer, and then re-bond. B): Cut out an approx 2'x 2' piece of the skin, (between the spar and ribs), then repair. Then perhaps increase spar/rib flange bonding area, then rebond the skin piece back in. However, if not strong enough, this may compromise the tortional rigidity offered by the single piece skin - or if too strong, may create a stress point during normal wing deflection. (???) C): Just open/clean the crack, fill the crack/hole with Hysol (fuel impervious), then repair externally with appropriate bids and finish to a smooth profile. p.s. For those who know me, this is not my ES (thankfully).