Return-Path: Received: from hotmail.com ([216.33.237.109]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with SMTP id com for ; Wed, 15 Dec 1999 00:27:36 -0500 Received: (qmail 83318 invoked by uid 0); 15 Dec 1999 05:32:20 -0000 Received: from 204.215.229.45 by www.hotmail.com with HTTP; Tue, 14 Dec 1999 21:32:19 PST Message-ID: <19991215053220.83317.qmail@hotmail.com> From: "ED SIKORA" To: lancair.list@olsusa.com Subject: LC235 ventral fin... Date: Tue, 14 Dec 1999 21:32:19 PST X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I'm aware that in an effort to increase the vertical stab/rudder area some 235's have a built up (down) ventral fin starting behind baggage bulkhead enging up in a 3"-4" extension of the rudder. My plane is upside down for nose gear hydraulic work and though it would be a good time to start planning for this. Can any of the 235 drivers that added this fin tell me any details of the construction (dimensions/materials/#of layups etc) they used. You can reply directly to my e-mail. Thanks in advance. -Ed Sikora LC235 (maybe 290) >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>