Return-Path: Received: from spider.innercite.com ([158.222.1.5]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Sat, 2 Oct 1999 01:23:59 -0400 Received: from innercite.com (plvpm3d-32-199.innercite.com [158.222.32.199]) by spider.innercite.com (8.9.1b+Sun/8.8.5) with ESMTP id WAA03481 for ; Fri, 1 Oct 1999 22:27:57 -0700 (PDT) Message-ID: <37F598B7.9944211F@innercite.com> Date: Fri, 01 Oct 1999 22:31:35 -0700 From: Steve & Claudette Colwell Reply-To: colwell@innercite.com Organization: Ms Colwell CC: lancair.list@olsusa.com Subject: Re: Fuel Selector location on LNC2 References: <19990930043129.AAA25865@truman.olsusa.com> <011601bf0b6b$21616360$11c295cf@bill> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> My 3/8" lines run thru the center of the main spar web (and thru 1/4" x 2" tapered phenolic with Don Goetz approval) along the front of the main spar to a planned location of the fuel valve above the main spar. The advantages are: 1. the fuel line is up hill all the way to the valve so no water or air can be trapped. (air can trap in a gascolator and push the fuel level BELOW the screen. Yep, fuel will pass thru a fine screen that will not pass air due to surface tension). 2. Water can not trap in a low area of line. 3. this is a short, uncluttered route. 4. it allows mounting of the gascolator (in my case a large Purolator gas filter per Glasair) above the selector valve and behind the firewall which gets the filter and drain valve away from the bottom of the airplane where it could get bashed by a gear up. I have details on the Purolator Filter per Glasair if anyone is interested. Steve [Steve, could you forward me a few photos of your fuel line routing along the main spar web. I've read your post several times and can't envision this based on your description. The aft side of the main spar web is already cluttered with control system routings, the front side of the main spar in the center section mates to the aft side of the wing spar extensions so running along the front of the c-section main spar doesn't work, and the only other logical location is along the forward side of the spar web on the wing spar extensions. If that's the case, how do you get the fuel line up there essentially through the spar web. It's a bit confusing. If photos are inconvenient, a sketch or two would also suffice. Thanks. ] >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html