Return-Path: Received: from marvkaye.olsusa.com ([205.245.9.245]) by truman.olsusa.com (Post.Office MTA v3.1.2 release (PO203-101c) ID# 0-44819U2500L250S0) with SMTP id AAA15019 for ; Wed, 18 Nov 1998 17:54:17 -0500 Message-Id: <3.0.3.32.19981118175107.02d3d75c@olsusa.com> Date: Wed, 18 Nov 1998 17:51:07 -0500 To: lancair.list@olsusa.com From: Marvin Kaye Subject: Re: Jack stands In-Reply-To: X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> It's been awhile since I closed out the wing center section so had to take a look at the location of the jack points to be sure... the way my closeout ribs went it, the inboard side of them aligns with the center of the jack points. I don't remember whether it was the manual that recommended that configuration or if I was smart enough to think about doing it on my own, but in looking at that installation I have no fears at all about using the jack points to lift the airframe. The BIDs which back them up extend upward onto the closeout rib and the main spar, so consequently are tied into the load transfer pads. There's no chance that I will ever deform the bottom of the fuselage using them for their intended purpose. I do agree, however, with those of you who have them situated in a spot where they don't get the advantage of the load transfer pads, closeout ribs, and main spar for backup, that coming up with a way to balance the loading across the bottom of the fuse to a good solid location (ie, main spar) is probably very prudent. I also agree with Bob J. that considering the ultimate purpose of the pads and not only their intermediate use as support points during construction should be the prime motivation and guiding light in coming up with a jacking system.