Return-Path: Received: from marvkaye.olsusa.com ([205.245.9.223]) by truman.olsusa.com (Post.Office MTA v3.1.2 release (PO203-101c) ID# 0-44819U2500L250S0) with SMTP id AAA3256 for ; Sat, 10 Oct 1998 09:53:27 -0400 Message-Id: <3.0.3.32.19981010095256.00716770@olsusa.com> Date: Sat, 10 Oct 1998 09:52:56 -0400 To: lancair.list@olsusa.com From: Marvin Kaye Subject: Re: 320 fuel system reply X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Bill Harrellson, you wrote: "I also added a crossflow valve" and I'm hoping that you'll expand a little on the location of that valve relative to the fuel selector and electric pumps. I'm following this thread (and the one about electrical systems, especially discussions of essential bus considerations) as I'm planning on eliminating the header tank, wetting the wings to the tips, and using 3/8" tubing for the plumbing as well, so will be relying on electrical pumps exclusively thanks to the pressure requirements of fuel injection... needless to say, anything I can learn to insure that my fuel system has adequate redundancy is very important to me. I'm looking forward to hearing some more.