Received-SPF: none
 receiver=logan.com; client-ip=68.230.240.59; envelope-from=taspilot@cox.net
Message-ID: <20081204172504.5Z2F6.409183.imail@eastrmwml43>
Date: Thu, 4 Dec 2008 17:25:04 -0500
From:  <taspilot@cox.net>
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Subject: Re: [FlyRotary] Re: Fuel system
Cc: Ernest Christley <echristley@nc.rr.com>
In-Reply-To: <list-3330302@logan.com>
MIME-Version: 1.0
Content-Type: text/plain; charset=utf-8
Content-Transfer-Encoding: quoted-printable
Sensitivity: Normal

Please remove me from your mailing lists.
taspilot@cox.net

---- Ernest Christley <echristley@nc.rr.com> wrote:=20
Al Gietzen wrote:
>
> Charlies' suggestion of the Facet transfer pump is what I've been=20
> using. I use a 'T' in the fuel return line to the main tank for the=20
> transfer pump so it didn't even require an additional fitting in the=20
> tank (above what is necessary for EFI). The Facet has a check valve=20
> function internally.
>
> There really is not a simpler system that I am aware of.
>
> Well; there is, but of course it is dependant on air frame design. My=20
> Velocity has gravity feed from both mains to a 3 gallon sump, gravity=20
> feed from sump to the EFI pump; regulator return to the sump. Now=20
> that=E2=80=99s simple.
>
> Al G
>
I think I may have you beat, Al.
My single 50gal tank has two outlets that T into a filter/water=20
separator. The exit is of the filter feeds two EFI pumps. A independent=20
gravity feed T's off in front of the filter...just in case.


--
Homepage:  http://www.flyrotary.com/
Archive and UnSub:   http://mail.lancaironline.net:81/lists/flyrotary/List.=
html