X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from mx1.magmacom.com ([206.191.0.217] verified) by logan.com (CommuniGate Pro SMTP 5.0c2) with ESMTPS id 718120 for flyrotary@lancaironline.net; Sun, 11 Sep 2005 01:09:27 -0400 Received-SPF: none receiver=logan.com; client-ip=206.191.0.217; envelope-from=pcasson@sasktel.net Received: from mail3.magma.ca (mail3.magma.ca [206.191.0.221]) by mx1.magmacom.com (8.13.0/8.13.0) with ESMTP id j8B58glC016244 for ; Sun, 11 Sep 2005 01:08:43 -0400 Received: from [192.168.2.203] (69-11-16-227.regn.hssx.sasknet.sk.ca [69.11.16.227]) (authenticated bits=0) by mail3.magma.ca (8.13.0/8.13.0) with ESMTP id j8B58dHg029409 (version=TLSv1/SSLv3 cipher=DHE-RSA-AES256-SHA bits=256 verify=NOT) for ; Sun, 11 Sep 2005 01:08:41 -0400 Message-ID: <4323BBDF.9000404@sasktel.net> Date: Sat, 10 Sep 2005 23:08:47 -0600 From: Perry Casson User-Agent: Mozilla Thunderbird 1.0 (Windows/20041206) X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: mystery inflight fuel pressure drop References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit Had a small issue on my last flight that I can not explain - anyone care to venture a guess what was going on? I was hmmmm-ing along at 7500' on friday about 60 minutes into a 2 hour flight when my EIS low fuel pressure alarm went off and fuel pressure had dropped to 29 psi (alarm set at 30 psi) and the engine went a bit lean. I switched on my backup pump and fuel pressure instantly went back to the normal 38 psi. Flew like that for a couple minutes and then decided to do I bit of investigation so I turn the backup pump back off but the fuel pressure remain at the normal 38 psi for the rest of the flight. No other problems other than I seem to be running a bit leaner than normal for a 12 o-clock setting on the EC-2 mixture control. My install is pretty much a clone of Tracy's pre-Renisis fuel system other than I've got a high wing (Glastar). Feed and return from left tank, fuel line y after a fuel shutoff valve, inline fuel filters upstream of parallel Federal Mogul pumps mounted on cockpit side of firewall, using stock 89 RX-7 pressure regulator, 88 NA Injectors, no damper. I've been try to come with a explanation that would account for such a issue and other than the fuel pressure regulator may have got stuck and the extra flow from turning on the second pump unstuck it. Perry Casson