X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Thu, 17 Feb 2011 11:16:00 -0500 Message-ID: X-Original-Return-Path: Received: from mout.perfora.net ([74.208.4.194] verified) by logan.com (CommuniGate Pro SMTP 5.4c2o) with ESMTP id 4873750 for lml@lancaironline.net; Thu, 17 Feb 2011 11:12:57 -0500 Received-SPF: none receiver=logan.com; client-ip=74.208.4.194; envelope-from=david@fahrencorp.com Received: from winxedgeus01.exchange.xchg (winxedgeus01.lxa.perfora.net [172.23.130.53]) by mrelay.perfora.net (node=mrus3) with ESMTP (Nemesis) id 0MYfb0-1PdRGI3X4E-00VpLo; Thu, 17 Feb 2011 11:12:21 -0500 Received: from winxhubus02.exchange.xchg (172.23.130.14) by winxedgeus01.exchange.xchg (172.23.130.53) with Microsoft SMTP Server (TLS) id 8.3.83.0; Thu, 17 Feb 2011 11:11:57 -0500 Received: from winxbeus17.exchange.xchg ([172.23.130.77]) by winxhubus02.exchange.xchg ([172.23.130.14]) with mapi; Thu, 17 Feb 2011 11:11:56 -0500 From: David Williams X-Original-To: Lancair Mailing List X-Original-Date: Thu, 17 Feb 2011 11:11:57 -0500 Subject: RE: [LML] De lamination and crack Thread-Topic: [LML] De lamination and crack Thread-Index: AcvOPWapK1kMK4giQ3aCWIk5iu9RIgAf6hew X-Original-Message-ID: References: In-Reply-To: Accept-Language: en-US Content-Language: en-US X-MS-Has-Attach: X-MS-TNEF-Correlator: acceptlanguage: en-US x-provags-id: V02:K0:LoGiCnFQf3bAUNB1fr622A/2YmdcY/CteYq+hqiqLMx 8mr4UYNt2nrpszzoSA5vmuuRI6Di7and7o0TvOC5cDeOveMW/R vsDM45AZgRTIUpnFeYhpkhdx/nNqwPJN4B2QoZxFbxakL0+hTk 2gVn7uUcNfZqyWfeu3VyPX0Nv27mhkmHlrK3mw4VnJBe481eT Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable MIME-Version: 1.0 X-Original-Return-Path: david@fahrencorp.com Best composite engineer; Sonja Englert www.caro-engineering.com/ -----Original Message----- From: Lancair Mailing List [mailto:lml@lancaironline.net] On Behalf Of Roge= r Iverin Sent: Wednesday, February 16, 2011 5:56 PM To: lml@lancaironline.net Subject: [LML] De lamination and crack Gents, On the fuselage inside under the left window I discovered a crack 5 in long= . Seems like it have been tried to hide with an "high speed vibration mod" May this be a sign for a de-lamination and possible affect the hole fuselag= e ? Anyone who know how to fix the crack and check for delamination ?? A/C currently located West Palm Beach. Best regards Roger Iverin -- For archives and unsub http://mail.lancaironline.net:81/lists/lml/List.html