X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Tue, 05 Jun 2007 22:35:59 -0400 Message-ID: X-Original-Return-Path: Received: from global.delionsden.com ([66.150.29.112] verified) by logan.com (CommuniGate Pro SMTP 5.1.9) with ESMTPS id 2086333 for lml@lancaironline.net; Tue, 05 Jun 2007 21:49:13 -0400 Received-SPF: none receiver=logan.com; client-ip=66.150.29.112; envelope-from=n103md@yahoo.com Received: from bmackey by global.delionsden.com with local (Exim 4.62) (envelope-from ) id 1HvkdT-00056Y-Rz for lml@lancaironline.net; Tue, 05 Jun 2007 21:48:31 -0400 Received: from 12.146.139.19 ([12.146.139.19]) (SquirrelMail authenticated user bmackey) by www.bmackey.com with HTTP; Tue, 5 Jun 2007 18:48:31 -0700 (PDT) X-Original-Message-ID: <27716.12.146.139.19.1181094511.squirrel@www.bmackey.com> X-Original-Date: Tue, 5 Jun 2007 18:48:31 -0700 (PDT) Subject: Hickman's Accident: NTSB Probable Cause Report From: "bob mackey" X-Original-To: lml@lancaironline.net User-Agent: SquirrelMail/1.4.8 MIME-Version: 1.0 Content-Type: text/plain;charset=iso-8859-1 Content-Transfer-Encoding: 8bit X-Priority: 3 (Normal) Importance: Normal X-AntiAbuse: This header was added to track abuse, please include it with any abuse report X-AntiAbuse: Primary Hostname - global.delionsden.com X-AntiAbuse: Original Domain - lancaironline.net X-AntiAbuse: Originator/Caller UID/GID - [32015 2012] / [47 12] X-AntiAbuse: Sender Address Domain - yahoo.com X-Source: X-Source-Args: X-Source-Dir: Dave Hickman's fatal accident remains a tragedy. With better training or skills, perhaps it would have been an "ordinary" engine out landing instead of a stall and uncontrolled descent. Why did the engine quit? If in fact selecting the high-boost switch caused the engine to flood and stop producing power, then there is a serious flaw in the fuel injection system of that particular engine and airframe. I've said it before and I'm saying it again... If varying the input fuel pressure (within a reasonable range) to the engine changes the fuel flow, then the fuel flow regulation system is flawed. In this case, you could say fatally flawed. The fuel flow should be determined by the mass airflow and the mixture setting. Not by which fuel pumps are on. If the fuel pumps in the system can exceed the pressures that the injection system is able to regulate, then those pumps should be removed. It's not just a matter of switch placement. There should be no auxiliary controls in the cockpit that cause the engine to quit working. The primary engine controls (e.g. magneto switch, fuel cutoff) are all the only ones that should stop the engine. If I needed a big 6-cylinder engine for my aircraft, I would not choose a fuel-injected Continental.