Return-Path: Received: from smtp9.gateway.net ([208.230.117.253]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Fri, 21 Jul 2000 00:43:32 -0400 Received: from oemcomputer (1Cust177.tnt3.coeur-dalene.id.da.uu.net [63.15.161.177]) by smtp9.gateway.net (8.9.3/8.9.3) with SMTP id AAA06646 for ; Fri, 21 Jul 2000 00:49:51 -0400 (EDT) Message-ID: <001401bff2d0$71eadd00$b1a10f3f@oemcomputer> Reply-To: "dfs" Reply-To: lancair.list@olsusa.com From: "dfs" To: "Lancair List" Subject: 235 control stick crossover weldment questions Date: Thu, 20 Jul 2000 21:59:25 -0700 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Ed, the next time I'll be able to get to the airport is Saturday morning (we're flying the Young Eagles here at Coeur d'Alene then) but I will look at my weldment and let you know unless someone else can tell you before that. I think (but at my age, memory is the second thing to go - and I don't remember what the first thing is) that the tabs lean forward while the sticks are approximately vertical. I believe it was done to provide more up elevator than down since the tabs come in contact with the spar when the stick is pushed to the forward limit of travel. Incidentally, I've got an early 235. Dan Schaefer >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>