Return-Path: Received: from m3.boston.juno.com ([205.231.100.198]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Wed, 31 Mar 1999 18:40:56 -0500 Received: (from earl_schroeder@juno.com) by m3.boston.juno.com (queuemail) id D63W5TDU; Wed, 31 Mar 1999 18:32:00 EST To: lancair.list@olsusa.com Date: Wed, 31 Mar 1999 17:35:15 -0600 Subject: LNC2 Fuel system plumbing Message-ID: <19990331.173519.12110.1.Earl_Schroeder@juno.com> From: Earl E Schroeder X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Marv, >>[Interesting approach, Earl... do you have the usual shutoff for the header, >>and if so, I assume you close that when pumping directly from the wings? >>And when you say that the tee at the firewall is 'valved' up to the header, >>is that what you're refering to? Anxious to hear more..... ] Yes the 'valved' is the usual valve from the header tank and is closed when pumping directly from the wings. I also have a rotometer in the line from the wings after the left-right-off valve and before the tee at the firewall. This probably will not be too useful since the Facet pumps pulse but I hope to be able to see 'bubbles' to verify an empty wing tank on purpose or by accident. BTW, I had to fabricate an extension to operate the on-off header valve since it is located too far forward to reach by hand. In retrospect, that probably should be within arm's reach but I couldn't figure out a way of doing it when using the std double sump on the header tanks and keeping the piping length minimum as well as the fitting count low. I may be over sensitive to vapor lock but I've heard some nasty stories from supposedly 'auto' gas users.... we can't even be absolutely sure what we are getting out of aviation pumps these days. Plus, if I have an unfortunate complete electrical failure, I wanted to give gravity and the engine driven pump a fighting chance of fueling the Lyc to a safe landing. Earl [Rotometer?? Can I assume (once again) that this is a type of flowmeter? Who makes it and where did you get it? I am inclined to keep everything in the fuel system as simple as possible, so will probably just run the transfer pumps to the header and be done with it. Although a crossover to level out wing fuel in case of a single transfer pump failure makes a lot of sense to me. Because I've mounted the hydraulic power pack on the firewall above the passenger footwell, my dump valve will be on the right side of the NG tunnel. That puts my header tank shutoff on the pilot's side, and I like your idea about the extension to operate it... would make it possible to mount the valve right at the sump and really keep that plumbing run short. Tomorrow I'll check that location to see if it isn't in the way of the rudder pedals. Thanks again for the tips. Much to think about. ]