Return-Path: Sender: (Marvin Kaye) To: lml Date: Fri, 26 Apr 2002 19:28:09 -0400 Message-ID: X-Original-Return-Path: Received: from moutvdomng1.kundenserver.de ([212.227.126.181] verified) by logan.com (CommuniGate Pro SMTP 3.5.9) with ESMTP id 1201562 for lml@lancaironline.net; Fri, 26 Apr 2002 10:21:11 -0400 Received: from [212.227.126.155] (helo=mrvdomng2.kundenserver.de) by moutvdomng1.kundenserver.de with esmtp (Exim 3.22 #2) id 1716ay-0000PD-00 for lml@lancaironline.net; Fri, 26 Apr 2002 16:21:08 +0200 Received: from [62.155.192.48] (helo=antje) by mrvdomng2.kundenserver.de with smtp (Exim 3.22 #2) id 1716ax-0003Et-00 for lml@lancaironline.net; Fri, 26 Apr 2002 16:21:08 +0200 From: "Rudolf Winter" X-Original-To: "'Lancair Mailing List'" Subject: position of after spar slow build IV wing X-Original-Date: Fri, 26 Apr 2002 16:20:40 +0200 X-Original-Message-ID: <000001c1ed2d$979489d0$fe63a8c0@antje> X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook CWS, Build 9.0.2416 (9.0.2910.0) Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V5.50.4522.1200 Please allow a question about positioning the after spar: My manual (page 5-29 rev 1 / 10-26-91) gives me the following dimension for positioning the after spar (L.E. front spar - aft face rear spar) BL 76 20 3/8", BL114 21 9/16", BL 171 17 7/8" This seems to be not ok. In my oppinion all dimension must be about 1" less. If I use the above dimension my rear spar would only rest half on the core material and would be half in the air !? Would anyone out there be so kind and check the dimensions and provide me with additional dimension from the wing T.E ? Is it possible to use Hysol (Araldite 2014) instead of epoxy flox to bond the spar? I have only the fast jeffco hardener and it would be no fun installing the spar with it... Is there a reason for closing the wing with epoxy flox instead of hysol (araldite)? Thank you in advance Rudolf Winter