Return-Path: Received: from baron.nii.net ([209.113.172.16]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Wed, 8 Nov 2000 10:02:51 -0500 Received: from nii.net (xcom33.nii.net [209.113.173.97]) by baron.nii.net (8.9.3/8.9.3) with ESMTP id KAA06640 for ; Wed, 8 Nov 2000 10:10:22 -0500 Message-ID: <3A096B9B.7B45877@nii.net> Date: Wed, 08 Nov 2000 10:05:00 -0500 From: "Angier M. Ames" Reply-To: alphadog@nii.net Reply-To: lancair.list@olsusa.com Organization: Alpha Delta Research To: lancair.list@olsusa.com Subject: Re: Carbinge or aluminum References: <20001108055017.AAA1936@ns1.olsusa.com> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Hi John et al, How would one apply this hinge to the inside top and bottom cowling and at the same time, prevent adhesive from migrating into and between the two hinge halves and bonding both together? I think it would be very helpful if one of you could describe the method for attaching aluminum and/or carb hinges to the cowling halves and the cowling rear sides and top, to the fuselage. Of course, all of this presumably would be done with engine/prop/spinner in place and with little or no opportunity to put either your hands or eyeballs in there to see or do something. What am I missing here? Angier Ames >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>