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, 5 Apr 2000 00:43:12 -0400 Received: from nii.net (xcom75.nii.net [209.113.173.139]) by baron.nii.net (8.9.3/8.9.3) with ESMTP id AAA01393 for ; Wed, 5 Apr 2000 00:40:04 -0400 Message-ID: <38EAC335.F5983458@nii.net> Date: Wed, 05 Apr 2000 00:38:14 -0400 From: "Angier M. Ames" Reply-To: alphadog@nii.net Organization: Alpha Delta Research To: lancair.list@olsusa.com Subject: Re: 360 flap installation References: <20000405042825.AAA4591@ns1.olsusa.com> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I have taken the time to be sure that all three flap hinges are in the same plane (pun intended) but I'm wondering just how much this hinge alignment will change when the wing is loaded up in flight. It would seem that there is no way to avoid a binding situation in flight. Looks like this just goes with the territory and is part of the wearing in process. Would appreciate any comments on this issue. Angier Ames >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>