Return-Path: Received: from smtp3.gateway.net ([208.230.117.247]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Wed, 20 Oct 1999 03:35:19 -0400 Received: from oemcomputer (1Cust94.tnt1.coeur-dalene.id.da.uu.net [63.27.107.94]) by smtp3.gateway.net (8.9.3/8.9.3) with SMTP id DAA20173 for ; Wed, 20 Oct 1999 03:39:28 -0400 (EDT) Message-ID: <000b01bf1ace$94c09f20$5e6b1b3f@oemcomputer> Reply-To: "dfs" From: "dfs" To: "Lancair List" Subject: Standard Stabilizer vs MK-II Stabilizer Date: Wed, 20 Oct 1999 00:36:36 -0700 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> More comments on this subject follow: I have airframe #52 which naturally, has the original (small) stabilizer. It doesn't bother me much but one does have to mind the store while on cruise. To allow me to spend some time looking at a chart or relevant publication, I installed a wing leveler autopilot as I got tired of having the horizon tilt wildly while I checked the map. Now, things are much more civilized and the only thing that needs to be watched is the airplane's tendency to change pitch attitude somewhat as I fly along. With the small stabilizer, there is a tendency to divert a bit from trim speed. I haven't experimented with it to find out just how much the airplane would climb or dive as it only takes a touch of pressure to return things to straight and level. It's not much of a burden and becomes second nature after a reasonable amount of time. If you have a constant speed prop, it's a bit harder to detect the divergence - with a fixed pitch prop, you can hear the RPM change and you are alerted. Most important, in my mind, is the fact that I've expanded the envelope on N235SP to 10% above red-line and have experienced absolutely no tendency to flutter. Therefore, in the normal range of flight speeds, I believe I'm staying very safe. The amount of work required to retrofit the larger tail, from my viewpoint theregore, isn't worth the effort. Dan Schaefer >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html