Return-Path: Received: from [216.52.245.18] (HELO ispwestemail1.aceweb.net) by logan.com (CommuniGate Pro SMTP 4.1.5) with ESMTP id 2639285 for flyrotary@lancaironline.net; Thu, 16 Oct 2003 12:17:25 -0400 Received: from ispwest.com (unverified [127.0.0.1]) by ispwestemail1.aceweb.net (Vircom SMTPRS 2.1.268) with ESMTP id for ; Thu, 16 Oct 2003 09:23:49 -0700 Message-ID: <4d6b2de091564090bbbbc44ef70c671e.wschertz@ispwest.com> X-EM-APIVersion: 2, 0, 1, 0 X-Priority: 3 (Normal) From: "Bill Schertz" To: "Rotary motors in aircraft" Subject: Re: [FlyRotary] Fwd: Fuel systems Date: Thu, 16 Oct 2003 09:23:49 -0700 MIME-Version: 1.0 Content-type: text/plain; charset=US-ASCII Content-Transfer-Encoding: quoted-printable Joe, Regarding this part of your question, it is most likely that the fuel will N= OT divide equally if you T the returns=2E Not a good idea, as small changes = in pressure drop/line length, etc=2E will affect the fuel distribution, and = you may not know where the fuel is=2E Bill Schertz KIS Cruiser # 4045 ----- Original Message ----- From: Joseph Berki >>Is there any way to divide the fuel return so it can be=20 > > returned to both tanks? If you tee the return lines does the fuel divid= e=20 > > evenly?=20