Return-Path: Received: from imo13.mx.aol.com ([198.81.17.3]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Mon, 14 Jun 1999 10:48:11 -0400 Received: from RWolf99@aol.com (4241) by imo13.mx.aol.com (IMOv20) id kJJDa05537 for ; Mon, 14 Jun 1999 10:50:27 -0400 (EDT) From: RWolf99@aol.com Message-ID: <7299f277.249670b2@aol.com> Date: Mon, 14 Jun 1999 10:50:26 EDT Subject: Control Surface Balancing To: lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> In a message dated 6/13/99 9:48:51 PM, you wrote: <> NO! NO! NO! Control surface balancing is done to prevent flutter. Please don't even THINK about ignoring this. While there may be an impact to the stick-force-per-G curve, as Ed suggests, the primary purpose of balancing the movable control surfaces.is to keep the airplane in one piece by preventing flutter. The bob-weight is the thing that increases the stick-force-per-G. Note that "irreversible surfaces" (ones where the aerodynamic load cannot change the surface position) do not require balancing. Flaps are one example. Hydraulically-boosted control surfaces are another, but there aren't any of those in Lancairs ..... yet! - Rob Wolf >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html