Return-Path: Received: from imo27.mx.aol.com ([198.81.17.71]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Tue, 12 Jan 1999 01:57:43 -0500 Received: from RWolf99@aol.com by imo27.mx.aol.com (IMOv18.1) id 6SLCa06037 for ; Tue, 12 Jan 1999 01:58:50 -0500 (EST) From: RWolf99@aol.com Message-ID: <73f9e643.369af2aa@aol.com> Date: Tue, 12 Jan 1999 01:58:50 EST To: lancair.list@olsusa.com Subject: Cockpit Closeout Rib 3-BID X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Pine - The manual states to use 3-BID at the rib-fuselage junctures. This point is not clearly stated, I'll admit, but it does say 3-BID. The illustration is rather vague since it doesn't show that upper area you're referring to. You should not add these until after you add the 12-BID load transfer pad. (Or if you do, don't put the 3-BID where the 12 BID will go later) Marv is correct -- a generous micro fillet is required. I found the layup to be quite easy when the aircraft is upside down. By the way, a goodly fraction of the LC20 wheel wells I've examined at Oshkosh -- maybe a third of them -- have forgotten to include the 3-BID layup. - Rob Wolf rwolf99@aol.com