Return-Path: Received: from imo-r10.mx.aol.com ([152.163.225.10]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-70783U4500L450S0V35) with ESMTP id com for ; Sat, 27 Jan 2001 08:55:25 -0500 Received: from N295VV@aol.com by imo-r10.mx.aol.com (mail_out_v29.5.) id k.dc.18aa6c6 (25312) for ; Sat, 27 Jan 2001 09:03:46 -0500 (EST) From: N295VV@aol.com Message-ID: Date: Sat, 27 Jan 2001 09:03:46 EST Subject: Re: Whoa, Holy Rear Spar To: lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> When I was building my LIV, I was surprised how flimsy the rear spar was before we glued in into the wing. I concluded at the time that the main function of the rear spar was to act as a termination to keep the trailing edges of the wing surfaces together--the added benefit of having a surface to attach some hinges was almost a secondary consideration, since the hinge attach points were always beefed up with lots of added bid layers. This being said, if you cut a hole in the wrong place along this flimsy rear web spar, simply add enough bid to more than make up for the thickness of the original, and extend the bid 4-6 inches on each side of the void. Fill the void with epoxy flox then, and put a 2 bid on the opposite side. I read your first thread without noticing that you said "rear" spar, and if it had been the main spar as I thought, you would have a very serious problem, indeed. But, as it turns out, you have a simple problem--easily corrected, and once you fix it, you should put it out of mind and sleep well at night. David Jones >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>