Return-Path: Received: from spider.innercite.com ([158.222.1.5]) by truman.olsusa.com (Post.Office MTA v3.1.2 release (PO203-101c) ID# 0-44819U2500L250S0) with ESMTP id AAA7311 for ; Sat, 10 Oct 1998 18:06:45 -0400 Received: from innercite.com (plvpm3a-32-85.innercite.com [158.222.32.85]) by spider.innercite.com (8.8.7/8.8.5) with ESMTP id PAA17532 for ; Sat, 10 Oct 1998 15:08:41 -0700 (PDT) Message-ID: <361FDABC.2278A867@innercite.com> Date: Sat, 10 Oct 1998 15:07:57 -0700 From: Steve Colwell Reply-To: colwell@innercite.com Organization: Ms Colwell To: a Subject: Old 320/360 fuel system drawbacks X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> With all the debate on fuel system varieties along with the pros and cons, heres what I have and why on my 360-slobuild. NO header, 1. burn and fill changes pitch trim constantly 2. manually requires refilling too frequently (I have heard several stories of "washing the windshield" when they forgot to turn off the pump in time.) 3. automatic refilling too complex 4. in a previous A/C many of the fatals were caused by ruptured headers (if I really wanted the extra fuel I would put in a 3 way valve and use the header as the last fuel burned) Wing fuel out to the tip ribs because 4 hours in the saddle is as much fun as I can stand. A baffle rib with flapper valve at BL-60 to avoid unporting a low tank in the pattern. I used a friends idea and routed the 3/8 fuel pickup line thru the main spar webs about BL-54(with Don Goetz blessing) then forward of the main spar to aft of the nose gear tunnel. This is the shortest run with the fewest bends and no low spots for water to accumulate. A right-left-off fuel valve and probably a super fine fuel filter from Airflow Performance or Lancair in lieu of a gascolator since I plan to sump the mains a lot. This is similar to the stock RV-6 system I am flying with and is as KISS as I can think of . Steve