Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Thu, 04 Dec 2003 21:52:26 -0500 Message-ID: X-Original-Return-Path: Received: from [32.97.166.32] (HELO prserv.net) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2784088 for lml@lancaironline.net; Thu, 04 Dec 2003 20:56:57 -0500 Received: from b8p5r1 (slip-12-65-198-55.mis.prserv.net[12.65.198.55]) by prserv.net (out2) with SMTP id <2003120501565620206gte3ue>; Fri, 5 Dec 2003 01:56:57 +0000 From: "Larry Henney" X-Original-To: "'Lancair Mailing List'" Subject: RE: [LML] Bonding rear windows L2C X-Original-Date: Thu, 4 Dec 2003 20:04:58 -0600 X-Original-Message-ID: <000001c3bad4$336388a0$37c6410c@b8p5r1> MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.2627 Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 Mike, My aft windows have 1" bond top and bottom and about 0.6" bond for/ aft. The internal glass combined with the hysol plexi to e-glass bond has managed to hold together for 450 hours. You might confirm with Lancair your plan. If there is perhaps some fuselage strength through the window issue they'd be able to let you know. Otherwise, I'd imagine you would be fine. Larry Henney N360LH PS: As an ex 125 Instructor, I'd love to hear the status of the fleet (fuel, parts, flying hours, morale, etc).