X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sun, 07 Jul 2013 10:50:43 -0400 Message-ID: X-Original-Return-Path: Received: from mail-we0-f169.google.com ([74.125.82.169] verified) by logan.com (CommuniGate Pro SMTP 6.0.5) with ESMTPS id 6363091 for lml@lancaironline.net; Sat, 06 Jul 2013 20:45:10 -0400 Received-SPF: pass receiver=logan.com; client-ip=74.125.82.169; envelope-from=jeffreyb.peterson@gmail.com Received: by mail-we0-f169.google.com with SMTP id n57so2834878wev.14 for ; Sat, 06 Jul 2013 17:44:36 -0700 (PDT) MIME-Version: 1.0 X-Received: by 10.180.185.84 with SMTP id fa20mr26514365wic.49.1373157876586; Sat, 06 Jul 2013 17:44:36 -0700 (PDT) Received: by 10.194.124.72 with HTTP; Sat, 6 Jul 2013 17:44:36 -0700 (PDT) Reply-To: jbp@cmu.edu X-Original-Date: Sat, 6 Jul 2013 20:44:36 -0400 X-Original-Message-ID: Subject: Re: Header Tank in the 360 From: Jeff Peterson X-Original-To: Rob Murawski , Lancair mail list Content-Type: multipart/alternative; boundary=001a11c2404c745fa104e0e13b11 --001a11c2404c745fa104e0e13b11 Content-Type: text/plain; charset=ISO-8859-1 Hey Rob, If you scan the archive you will find this issue vigorously debated several times. Reminds me of the Mac vs PC debate (or Unix vs VMS for us old fogeys) (or Python vs C for younger guys). Most of us just keep repeating whatever argument validates the particular choice we selected. As you know, I put the fuel in the outer wing bays and use the header space for avionics. I have 42 gal usable. I put in slosh gates. I am very happy. reasons for my choice: -There are, oh maybe a million, airplanes configured this way....most aircraft designers make this choice. -Lancair switched to this system with the Legacy. -If I have an off-airport landing and break things, I would rather not get doused with fuel. -In the header system, if you leave a facet pump on too long you pump fuel overboard. -In the header system if you forget to turn on the facet pump every 20 min. the engine dies. -Yes, these last two problems can be fixed by automating transfers...but that adds a system with its own failure modes. -The headers space is really useful for ahrs, rf splitters, pitot-static manifolds, misc. circuits, regulators etc. To each his own....but the fuel-in-the-wings system is in fact a very reasonable choice. -- Jeff Peterson 99.8% --001a11c2404c745fa104e0e13b11 Content-Type: text/html; charset=ISO-8859-1 Content-Transfer-Encoding: quoted-printable Hey Rob,

If you scan the archive you will find this issu= e vigorously debated several times.

Reminds me of = the Mac vs PC debate (or Unix vs VMS for us old fogeys) (or Python vs C for= younger guys). =A0
Most of us just keep repeating whatever argument validates the particu= lar choice we selected.

As you know, I put the fue= l in the outer wing bays and use the header space for avionics.
I have 42 gal usable. =A0I put in slosh gates. I am very happy.
<= br>
reasons for my choice:

-There are, o= h maybe a million, airplanes configured this way....most aircraft designers= make this choice.
-Lancair switched to this system with the Legacy.
-If I have= an off-airport landing and break things, I would rather not get doused wit= h fuel.
-In the header system, if you leave a facet pump on too l= ong you pump fuel overboard.
-In the header system if you forget to turn on the facet pump every 20= min. the engine dies.
-Yes, these last two problems can be fixed= by automating transfers...but that adds a system with its own failure mode= s.
-The headers space is really useful for ahrs, rf splitters, pitot-stat= ic manifolds, misc. circuits, regulators etc.

To e= ach his own....but the fuel-in-the-wings system is in fact a very reasonabl= e choice.

--=A0
Jeff Peterson
99.8%=A0
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