Return-Path: Received: from [24.50.193.34] (HELO dell) by logan.com (CommuniGate Pro SMTP 4.0.5) with ESMTP-TLS id 2013044 for lml@lancaironline.net; Sat, 08 Feb 2003 20:41:28 -0500 Message-ID: <003401c2cfdc$5c771ce0$053b3690@dell> From: "Root" To: "Lancair Mailing List" Subject: Fw: LNC2 extended wing tanks. Date: Sat, 8 Feb 2003 20:41:25 -0500 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1106 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 From: "Jeffrey Peterson" Lorn, My motivation for the wing tank extension is to get rid of the header tank. That also eliminates the facet pump system. I will use a 2-way fuel valve. Like the Legacy. I dont like fuel above my lap. Could turn a minor accident into a very bad day. I have seen two 360s done this way and was impressed. Easy access to the avionics is an added feature. -Jeff -- Jeff Peterson Dept. of Physics Carnegie Mellon University Pittsburgh PA 15213 phone: 412-268-2785 fax 412-681-0648