Return-Path: Sender: "Marvin Kaye" To: lml@lancaironline.net Date: Sun, 13 Mar 2005 23:26:54 -0500 Message-ID: X-Original-Return-Path: Received: from ispmxmta09-srv.alltel.net ([166.102.165.170] verified) by logan.com (CommuniGate Pro SMTP 4.3c2) with ESMTP id 791981 for lml@lancaironline.net; Sun, 13 Mar 2005 22:18:41 -0500 Received-SPF: neutral receiver=logan.com; client-ip=166.102.165.170; envelope-from=micah@froese.com Received: from DDSV6921 ([151.213.88.138]) by ispmxmta09-srv.alltel.net with ESMTP id <20050314031756.IDFD4937.ispmxmta09-srv.alltel.net@DDSV6921> for ; Sun, 13 Mar 2005 21:17:56 -0600 X-Original-Message-ID: <001101c52844$68da20a0$6401a8c0@mcm.local> From: "Micah Froese" X-Original-To: "Lancair Mailing List" References: Subject: Legacy fuel reurn line routing X-Original-Date: Sun, 13 Mar 2005 22:17:47 -0500 MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1409 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1409 Does anyone out there see any advantageous way to route the fuel return line coming fron the stub wing? I have a choice between putting them throught the center console or along the side of the fuselage forward and then across to the middle once they are by the spar. I have run my hydraulic lines under the passenger seat as per t he updated manual. Micah Legacy