Return-Path: Received: from marvkaye.olsusa.com ([205.245.9.102]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with SMTP id com for ; Mon, 25 Jan 1999 09:45:09 -0500 Message-Id: <3.0.3.32.19990125094404.0393fb98@olsusa.com> Date: Mon, 25 Jan 1999 09:44:04 -0500 To: lancair.list@olsusa.com From: Marvin Kaye Subject: LC20 Pitch Sensitivity X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Posted for Greg Nelson : Several years ago a builder in California (I don't remember his name) designed and tested a pitch enhancement modification to his small-tailed 360 airplane which he called a "strake". The design of this strake was simply to move (or "fair") the INNERMOST leading edge of the horizontal stab forward some distance so as to increase the total surface area of the stab and also to capture more air farther forward than does the original design thus to increase the effectiveness of the the small tail. He claimed considerable improvements in slow speeds and approaches but does he still? At the time, this seemed like the definitive solution for all small-tailed Lancairs; a quick and inexpensive improvement in pitch stability. Who was that builder? What has become of this modification? Do any of you have additional, helpful information on the strake?