Return-Path: Received: from baron.nii.net ([209.113.172.16]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Tue, 12 Jan 1999 23:33:36 -0500 Received: from nii.net (xcom50.nii.net [209.113.173.114]) by baron.nii.net (8.8.5/8.8.5) with ESMTP id XAA31798 for ; Tue, 12 Jan 1999 23:35:02 -0500 Message-ID: <369C2425.16BE0BE6@nii.net> Date: Wed, 13 Jan 1999 00:42:13 -0400 From: "Angier M. Ames" Organization: Alpha Delta Research To: lancair.list@olsusa.com Subject: Re: Horizontal stabilizer incidence References: <19990112053249.AAA22953@truman.olsusa.com> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> When you get around to attaching the stab, it is worth stating that the stabilizer incidence as it relates to a LEVEL fuselage is absolutely irrelevant.(IMO). The only measurement that matters is the stab incidence relative to the wing.The fuselage is just along for the ride and provides a practical means for fixing(permanently), the stab/wing incidence. Angier Ames