Return-Path: Received: from burgoyne.com ([209.197.0.8]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Fri, 23 Apr 1999 09:41:46 -0400 Received: from clkeller.burgoyne.com (pmb38.burgoyne.com [209.197.2.91]) by burgoyne.com (8.9.1/8.9.1) with SMTP id HAA05444 for ; Fri, 23 Apr 1999 07:44:08 -0600 Message-ID: <372078A8.1E38@burgoyne.com> Date: Fri, 23 Apr 1999 07:42:00 -0600 From: "C.L.Keller" To: lancair.list@olsusa.com, lancair.list@olsusa.com Subject: 320 SFB Center Section attachment X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I'm facing the task of attaching the wing center section to the fuselage on my 320 SFB. I've had the center section in place, checked and corrected all levels and alignments, and am now facing the job of gluing it in place. The manual says to use Hysol on the glass-to-glass bond lines and forward load transfer pad (main spar), and micro on the foam pads. My problem is that the forward glass-to-glass bond line, where the fuselage bottom overlaps the underside of the main spar, causes a very tight fit for the forward spar. To get it in place the aft end of the center section has to be raised while the main spar is tucked under the fuselage bottom (remember, everything is up-side-down), then lowered while the spar cap slides forward on the load transfer pads. Works fine, but if the load transfer pad and the spar cap have had Hysol applied, this motion will wipe the surface clean. Once the center section is in place it is so tight there is no chance of raising it to create a gap above the load transfer pad to work Hysol into place. Can anyone who remembers having attached their center section offer suggestions or comments about how they managed it? Charles Keller >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html