Return-Path: Received: from sphmgaab.compuserve.com ([149.174.177.151]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Mon, 11 Sep 2000 10:42:20 -0400 Received: (from mailgate@localhost) by sphmgaab.compuserve.com (8.9.3/8.9.3/SUN-1.9) id KAA18580; Mon, 11 Sep 2000 10:49:04 -0400 (EDT) Date: Mon, 11 Sep 2000 10:48:34 -0400 From: James Frantz Subject: AOA Port locations & Rudder cable Sender: James Frantz To: Marve Kay , Charles Patton Message-ID: <200009111048_MC2-B2E7-FAAA@compuserve.com> X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> To answer Charles Patton question, the preferred location for the AOA pressure taps is forward of the ailerons or in the winglet between 15 and 40% chord. In your case, the aileron bellcrank access panel might provide the best access with the ports located just aft of the main spar. Other locations are possible. BTW, would you consider loaning out your teflon rudder cable injection tool? I would pay for shipping and return it promptly. Thanks for pointing out your article in the Lancair Network News. A smooth rudder operation is just around the corner. Jim >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>