Return-Path: Received: from marvkaye.olsusa.com ([205.245.9.165]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with SMTP id com for ; Fri, 9 Jul 1999 11:16:57 -0400 Message-Id: <3.0.3.32.19990709112008.009fecd0@olsusa.com> Date: Fri, 09 Jul 1999 11:20:08 -0400 To: lancair.list@olsusa.com From: Marvin Kaye Subject: Re: Severe Pitch Moment with Flap Extension X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Posted for "Paul A. Nafziger" : Thanks Bob & Tom. I think his stick forces are way above 5-10 pounds. He flew the 320 at Redmond to compare and said the pitching moment was much, much lower. The forces needed to counteract the moment are so high that he's afraid of damaging something if he extends more flaps. He has removed the spring trim system and has a large electric trim tabs on all three axes. Not sure what speed he's been using for flap limit speed, but I know it's not high. I'll check. I've thought of possible control binding or interference, but can find nothing on the ground. Maybe our next step is for me to chase him.... Naf N7PN (still working) [Naf... in the future, please quote back the subject of the post you are replying to, not >"Re: lancair.list V1 #42". This is why I reposted your message on your behalf. Thanks. ] >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html