X-Virus-Scanned: clean according to Sophos on Logan.com X-SpamCatcher-Score: 10 [X] Return-Path: Sender: To: lml@lancaironline.net Date: Tue, 08 May 2007 09:31:01 -0400 Message-ID: X-Original-Return-Path: Received: from web51007.mail.re2.yahoo.com ([206.190.38.138] verified) by logan.com (CommuniGate Pro SMTP 5.1.8) with SMTP id 2031924 for lml@lancaironline.net; Tue, 08 May 2007 08:32:07 -0400 Received-SPF: none receiver=logan.com; client-ip=206.190.38.138; envelope-from=bu131@swbell.net Received: (qmail 2818 invoked by uid 60001); 8 May 2007 12:31:14 -0000 DomainKey-Signature: a=rsa-sha1; q=dns; c=nofws; s=s1024; d=swbell.net; h=X-YMail-OSG:Received:Date:From:Subject:To:In-Reply-To:MIME-Version:Content-Type:Content-Transfer-Encoding:Message-ID; b=X5dgQ9kqkf4Ik054qFuXsn7yQf9UcQ37HAbjy66CQ7uD08nB2wE62KhDFiU6fqw7Y+96T5D3L7YKMfXuZJMLc1f7B8C6urNGLUszT7NohQasHo96Nck/5lK4LDNUrstXeZukEbYFnZZgbOVwLp2VtRddYSSlYVSwEThN3co/I30=; X-YMail-OSG: gpM1k1AVM1kEqui8HQ6L1ryUHISk8shTWx7BTYxHkQFH3H1Qm7Dk0hWI8SMGAtZ8jJ8fwDlXHg-- Received: from [208.189.200.2] by web51007.mail.re2.yahoo.com via HTTP; Tue, 08 May 2007 05:31:14 PDT X-Original-Date: Tue, 8 May 2007 05:31:14 -0700 (PDT) From: Dr Andre Katz Subject: Re: [LML] Why is there fuel? X-Original-To: Lancair Mailing List In-Reply-To: MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="0-808762603-1178627474=:1942" Content-Transfer-Encoding: 8bit X-Original-Message-ID: <378306.1942.qm@web51007.mail.re2.yahoo.com> --0-808762603-1178627474=:1942 Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: 8bit my IV-P will quit any time over 14,000 feet (at that altitude i always have the low fuel pump on) unless momentarily and for 3 seconds before switching tanks i turn the high fuel pump on, the short surge at 23,000 feet is scary when the engine quits and everything goes dead, the fuel mixture gets messed up and for a couple of seconds the engine gets very leannnnnnnnnnnnnnnnnnn andres Kevin Stallard wrote: Hi all, Actually the question really is, why does the IO-550 require an electric fuel pump (besides priming/starting)? Why is there both a low boost and high boost pump? Is this only for backup, or are there more sinister aspects of fuel delivery in the IO-550 at play here? In talking with a friend of mine, he mentions that the Lycoming io360 only has a low pressure fuel pump. I remember a discussion about the TIO-550 and the fuel pump needs to be turned on above 10,000 feet. Why is this? This person I’ve been speaking to about this seemed to think it was to overcome vapor lock. Why doesn’t the IO-360 need something like this? Does the IO-550 need to be treated in the same way? Thanks Kevin --0-808762603-1178627474=:1942 Content-Type: text/html; charset=iso-8859-1 Content-Transfer-Encoding: 8bit
my IV-P will quit any time over 14,000 feet (at that altitude i always have the low fuel pump on) unless momentarily and for 3 seconds before switching tanks i turn the high fuel pump on, the short surge at 23,000 feet is scary when the engine quits and everything goes dead, the fuel mixture gets messed up and for a couple of seconds the engine gets very leannnnnnnnnnnnnnnnnnn
andres

Kevin Stallard <Kevin@arilabs.net> wrote:
Hi all,
 
Actually the question really is, why does the IO-550 require an electric fuel pump (besides priming/starting)? 
 
Why is there both a low boost and high boost pump?   Is this only for backup, or are there more sinister aspects of fuel delivery in the IO-550 at play here?  In talking with a friend of mine, he mentions that the Lycoming io360 only has a low pressure fuel pump.
 
I remember a discussion about the TIO-550 and the fuel pump needs to be turned on above 10,000 feet.   Why is this?  This person I’ve been speaking to about this seemed to think it was to overcome vapor lock.  Why doesn’t the IO-360 need something like this?  Does the IO-550 need to be treated in the same way?
 
Thanks
Kevin
 
 
 

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