X-Virus-Scanned: clean according to Sophos on Logan.com X-SpamCatcher-Score: 30 [X] Return-Path: Sender: To: lml@lancaironline.net Date: Thu, 26 Apr 2007 15:24:13 -0400 Message-ID: X-Original-Return-Path: Received: from tomts10-srv.bellnexxia.net ([209.226.175.54] verified) by logan.com (CommuniGate Pro SMTP 5.1.8) with ESMTP id 2011826 for lml@lancaironline.net; Thu, 26 Apr 2007 12:27:05 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.226.175.54; envelope-from=ian.crowe@sympatico.ca Received: from desktop ([69.159.77.95]) by tomts10-srv.bellnexxia.net (InterMail vM.5.01.06.13 201-253-122-130-113-20050324) with SMTP id <20070426162612.NVDZ1723.tomts10-srv.bellnexxia.net@desktop> for ; Thu, 26 Apr 2007 12:26:12 -0400 X-Original-Message-ID: <004701c7881f$b2b3a5b0$0d02a8c0@desktop> From: "Ian Crowe" X-Original-To: "Lancair Mailing List" Subject: Inspection panel installation X-Original-Date: Thu, 26 Apr 2007 12:26:52 -0400 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0044_01C787FE.2B64FCB0" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.3028 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.3028 This is a multi-part message in MIME format. ------=_NextPart_000_0044_01C787FE.2B64FCB0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable When building my a/c I seem to remember there was an instruction as to = how to cut out inspection panels and having done that to make and = position the fibre glass for the panel to butt up against as well as = carrying the anchor nuts for the fixing of the panel. This fibre glass = is epoxied to the fuselage, provides a seat for the panel around the = opening. Can anyone point me in the right direction in the manual for this = instruction? Please! Ian B. Crowe LNC 2 C-FKRO ------=_NextPart_000_0044_01C787FE.2B64FCB0 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
When building my a/c I seem to remember = there was=20 an instruction as to how to cut out inspection panels and having done = that to=20 make and position the fibre glass for the panel to butt up against as = well as=20 carrying the anchor nuts for the fixing of the panel.  This fibre = glass is=20 epoxied to the fuselage, provides a seat for the panel around the=20 opening.
 
Can anyone point me in the right = direction in the=20 manual for this instruction?  Please!
 
Ian B. Crowe
LNC 2 =20 C-FKRO
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