Return-Path: Sender: (Marvin Kaye) To: lml Date: Thu, 06 Feb 2003 18:29:43 -0500 Message-ID: X-Original-Return-Path: Received: from fire.phys.cmu.edu ([128.2.26.129] verified) by logan.com (CommuniGate Pro SMTP 4.0.5) with ESMTP id 2010886 for lml@lancaironline.net; Thu, 06 Feb 2003 12:05:08 -0500 Received: from localhost (jbp@localhost) by fire.phys.cmu.edu (8.11.6/8.11.6) with ESMTP id h16H51B13206 for ; Thu, 6 Feb 2003 12:05:02 -0500 X-Original-Date: Thu, 6 Feb 2003 12:05:01 -0500 (EST) From: Jeffrey Peterson X-Original-To: lancair mail list Subject: LNC2 extended wing tanks. X-Original-Message-ID: MIME-Version: 1.0 Content-Type: TEXT/PLAIN; charset=US-ASCII I have a partially completed 360, and have decided to extend the wing tanks. Unfortnately, the wings are already closed, with tank sealer applied. The previous owner built an access panel into the outboard wing compartment, which will now be the extension tank, so it will be fairly easy to install the new gas caps. I can seal the interior, and close the panel with sealer. The part I am unsure about is installing the two flow channels (one for fuel, one for vapor) that extend from the each current tank, passing through the aileron bell crank area, to the extension tanks. I was thinking of using 1.5 inch 6061 tubing for this, but I dont want the seals at the ends to crack with flexure. Or, i could lay up a carbon channel, but then i need figure out how to seal the inside of that channel. and I guess I need flapper valves. Has anyone out there faced this challenge? Any advice? -Jeff Peterson N273CK