Return-Path: Received: from imo19.mx.aol.com ([198.81.17.9]) by truman.olsusa.com (Post.Office MTA v3.1.2 release (PO203-101c) ID# 0-44819U2500L250S0) with ESMTP id AAA3597 for ; Sat, 14 Nov 1998 11:31:54 -0500 Received: from Sky2high@aol.com by imo19.mx.aol.com (IMOv16.10) id 8TSOa04682 for ; Sat, 14 Nov 1998 11:31:14 -0500 (EST) From: Sky2high@aol.com Message-ID: <1d92375c.364db052@aol.com> Date: Sat, 14 Nov 1998 11:31:14 EST To: lancair.list@olsusa.com Subject: Small tail 320 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Let me jump on the front of the small tail bandwagon. The small tail is no problem if it is built correctly. You must use the 3 inch bellcrank at the elevator and stiffer trim springs to compensate for the greater force required (this is a good thing). It is also beneficial to utilize Mr. Reichal's geared trim wheel. If it matters, my empty weight CG is 1/16 inch forward of the Lancair- recommended empty weight CG. I also use the S-TEC 50 autopilot with the pitch servo pushrod connected to the forward elevator pushrod just behind the seats. This setup has exhibited excellent altitude holding for hours of flying without re-trimming the elevator. One must pay attention during the landing phase. My current technique is to stabilize on final with almost full flaps and some power maintaining an attitude almost to touchdown. Then, slight power reduction combined with flare and, as soon as the wheels kiss the runway, immediate power reduction to idle. This technique is why I am installing the Angle-of-Attack indicator. In any event, the small tail is perfectly adequate to this task. Scott Krueger N92EX