Return-Path: Received: from imo25.mx.aol.com ([152.163.225.69]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Wed, 29 Dec 1999 09:47:04 -0500 Received: from RWolf99@aol.com by imo25.mx.aol.com (mail_out_v24.6.) id k.0.e6eea6ea (4330) for ; Wed, 29 Dec 1999 09:51:54 -0500 (EST) From: RWolf99@aol.com Message-ID: <0.e6eea6ea.259b7a0a@aol.com> Date: Wed, 29 Dec 1999 09:51:54 EST Subject: LNC2 Elevator Trim Sensitivity To: lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Having heeded the advice of those before me on this issue, I am installing a DPDT switch for my landing gear. One pole will be for the gear, and the other will switch the feed voltage (probably not the correct term) to the MAC servo. The plan is to run the servo at 12 Volts when the gear is down and some lesser voltage when the gear is up. This should provide reduced trim tab rates when at cruise, but a higher trim tab rate when the plane is slow, flaps are deploying, etc. I plan on starting with 5 Volts with gear up and refining this during flight test. This idea (multiple feed voltages) was originally published in the LNN newsletter, but incorporating it into the landing gear switch was not mentioned at that time. As you know, I'm not flying yet, so there will be no flight test report until the next millenium... - Rob Wolf >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>