X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Tue, 18 Apr 2006 12:26:44 -0400 Message-ID: X-Original-Return-Path: Received: from xproxy.gmail.com ([66.249.82.198] verified) by logan.com (CommuniGate Pro SMTP 5.0.9) with ESMTP id 1071718 for lml@lancaironline.net; Tue, 18 Apr 2006 03:08:24 -0400 Received-SPF: pass receiver=logan.com; client-ip=66.249.82.198; envelope-from=bakercdb@gmail.com Received: by xproxy.gmail.com with SMTP id t12so477061wxc for ; Tue, 18 Apr 2006 00:07:38 -0700 (PDT) DomainKey-Signature: a=rsa-sha1; q=dns; c=nofws; s=beta; d=gmail.com; h=received:message-id:date:from:to:subject:mime-version:content-type; b=nGaD8Ev0kAJi3b9jLM8xF4ZObCy/jqBESB3r0ZPQTaxaE6cHB92o0OS+ca5ibLPYTWLfzrEEvFY5cEzsqLLuK2mgbyLiZAtM8SIC/dAriDOQBizfNwQ0i+gbHYIBKSwiXHbEbcLOdCjGBFUjRtXAh3I9aNpHEBSOG/I9KmgGwQs= Received: by 10.70.124.7 with SMTP id w7mr4692927wxc; Tue, 18 Apr 2006 00:07:38 -0700 (PDT) Received: by 10.70.27.4 with HTTP; Tue, 18 Apr 2006 00:07:38 -0700 (PDT) X-Original-Message-ID: <175557b90604180007v4f46a291la97f1b3d8d7e3545@mail.gmail.com> X-Original-Date: Tue, 18 Apr 2006 08:07:38 +0100 From: "Clark Baker" X-Original-To: "Lancair Mailing List" Subject: Fuel Transfer MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_Part_11144_15423484.1145344058503" ------=_Part_11144_15423484.1145344058503 Content-Type: text/plain; charset=ISO-8859-1 Content-Transfer-Encoding: quoted-printable Content-Disposition: inline Terrence, You might look at the PP Avionics fuel controller. It automatically shuts off the pump and indicates when a tank is pumped dry by sensing the change in the current draw (I don't remember for sure). Very slick unit and used by several Lancair owners, including myself. I happen to use a Grand Rapid= s Technologies header tank fuel probe with hi/lo outputs to drive the sensing versus the standard optical probes. http://ppavionics.com/XFR.htm Regards, Clark Baker On 4/18/06, terrence o'neill wrote: > > To those who've been there-done that on early Lancairs -- request your > comments. I want a minimum-management on-off fuel supply. > For my L235 w/ IO320, I'm now running the fuel line from each wing tank > through a filter on each Facet pump, then from each pump -- both into an > open Tee, up to the header tank -- > Control of the Facet wingtank pumps' is on-off with an > optical level-sensor in the header, > to break or complete the plus-circuit 12VDC to each/both tanks' > power-on/off switches. > Left and right tank Facet pumps individual switches are normally left on, > and powered when a/c master is on. A red 'pumping' light is in the wing > tank pumps' power circuit, cycles on and off as sensor demands fuel for t= he > header. When light stays on, attention is called to the > How can power to the L and R wing tank Facet pumps automatically switch > off when the wing tanks are dry? > ------=_Part_11144_15423484.1145344058503 Content-Type: text/html; charset=ISO-8859-1 Content-Transfer-Encoding: quoted-printable Content-Disposition: inline
Terrence,
You might look at the PP Avionics fuel controller.  It automatica= lly shuts off the pump and indicates when a tank is pumped dry by sensing t= he change in the current draw (I don't remember for sure).  = Very slick unit and used by several Lancair owners, including myself. = I happen to use a Grand Rapids Technologies header tank fuel probe with hi= /lo outputs to drive the sensing versus the standard optical probes.
 
 
Regards,
Clark Baker

 
On 4/18/06, = terrence o'neill <troneill@c= harter.net> wrote:
To those who've been= there-done that on early Lancairs -- request your comments. I want a minim= um-management on-off fuel supply.
For my L235 w/ IO320= , I'm now running the fuel line from each wing tank through a  fi= lter on each Facet pump, then from each pump -- both into an open= Tee, up to the header tank --
Control of the Facet= wingtank pumps' is on-off with an optical level-sensor in the header,=  
to break or com= plete the plus-circuit 12VDC to each/both tanks' power-on/off switches= . 
Left and right tank = Facet pumps individual switches are normally left on, and powered when a/c = master is on.   A red 'pumping' light is in the wing tank pumps' = power circuit, cycles on and off as sensor demands fuel for the header= .   When light stays on, attention is called to the
How can power t= o the L and R wing tank Facet pumps automatically switch off = ;when the wing tanks are dry?   
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