Return-Path: Received: from fep13-svc.tin.it ([212.216.176.44]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Wed, 1 Dec 1999 21:45:47 -0500 Received: from tin.it ([212.216.215.195]) by fep13-svc.tin.it (InterMail vM.4.01.02.00 201-229-116) with ESMTP id <19991202025021.IQPQ14592.fep13-svc.tin.it@tin.it> for ; Thu, 2 Dec 1999 03:50:21 +0100 Message-ID: <3845DC1D.2513B42D@tin.it> Date: Thu, 02 Dec 1999 03:40:29 +0100 From: John F: Herminghaus Reply-To: catignano@tin.it To: Lancairlist Subject: Static Water X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> After having read the recent thread on static water, I plan to do the following on my IV-P. 1. Put a drain in the lowest section, easily reached by the pilot,and have an appropriate preflight check list item. 2. Run an alternate static source line to the nose wheel housing, or, should someone with more experience object to the nose wheel solution, back behind the pressure bulkhead. Any comments? John Herminghaus catignano@tin.it >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>