Return-Path: Received: from relay01.roc.ny.frontiernet.net ([66.133.182.164] verified) by logan.com (CommuniGate Pro SMTP 4.3c2) with ESMTP id 767643 for flyrotary@lancaironline.net; Wed, 02 Mar 2005 20:54:20 -0500 Received-SPF: pass receiver=logan.com; client-ip=66.133.182.164; envelope-from=canarder@frontiernet.net Received: from filter10.roc.ny.frontiernet.net (filter10.roc.ny.frontiernet.net [66.133.183.77]) by relay01.roc.ny.frontiernet.net (Postfix) with ESMTP id AC19436405F for ; Thu, 3 Mar 2005 01:53:34 +0000 (UTC) Received: from relay01.roc.ny.frontiernet.net ([66.133.182.164]) by filter10.roc.ny.frontiernet.net (filter10.roc.ny.frontiernet.net [66.133.183.77]) (amavisd-new, port 10024) with LMTP id 01263-10-88 for ; Thu, 3 Mar 2005 01:53:34 +0000 (UTC) Received: from [127.0.0.1] (67-137-89-39.dsl2.cok.tn.frontiernet.net [67.137.89.39]) by relay01.roc.ny.frontiernet.net (Postfix) with ESMTP id 0864636427F for ; Thu, 3 Mar 2005 01:53:33 +0000 (UTC) Message-ID: <42266E14.8010506@frontiernet.net> Date: Wed, 02 Mar 2005 19:53:24 -0600 From: Jim Sower User-Agent: Mozilla/5.0 (Windows; U; Windows NT 5.1; en-US; rv:1.7) Gecko/20040514 X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Re: [FlyRotary] Re: fuel cutoff valve necessary? References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit X-Antivirus: avast! (VPS 0509-3, 03/01/2005), Outbound message X-Antivirus-Status: Clean X-Virus-Scanned: by amavisd-new-20040701 (2.0) at filter10.roc.ny.frontiernet.net <... A throttle with a cutoff switch wired into it that would cut power to the pump after being pushed past a detent would accomplish three disjointed operations in one intuitive step, and leave the pilots throttle hand on the throttle ...> I think we're kind of gilding the lily here. Fuel pump switch(s) are used enough to be pretty easy to reach and fumbling for them cannot reasonably be classified as a significant distraction. OTOH automatic cutoff switches (hidden behind a detent or not) add several failure modes and a lot of complexity and expense - but no measurable benefit. I think we've got another one of those ten-cent tails wagging our forty-dollar dog ... Jim S. Ernest Christley wrote: > Ed Anderson wrote: > >> Ernest, I could be wrong, but seems I recall somewhere that FAA >> requires a >> fuel shut off valve. Someone else may know whether that is correct >> or not. >> For the reason you stated - Safety. >> >> Ed A >> >> >> > I don't doubt that it is so, Ed, but putting the edicts from Federal > agencies aside, I'd like to raise the question of whether it is safer. > I mentioned two instance where a valve for a single tank system would > be useful, an inflight fire and emergency landing prep. In both > instances, the pilot is required to remember to throttle back, turn > off the boost pump and then turn off the manual valve under the worst > of circumstances. Unless it is very well practiced, most pilots will > have to look around for the switches and knobs, taking their attention > away from other duties. If you're going in under partial power, you > may not be wanting to give up that power until very short final, > moving the list of task to the most dangerous times. A throttle with > a cutoff switch wired into it that would cut power to the pump after > being pushed past a detent would accomplish three disjointed > operations in one intuitive step, and leave the pilots thottle hand on > the throttle. > > Assuming that connections will be the weakest spot in any system, and > that there actually is a pump that blocks flow when there's no power > applied (I haven't tried to determine if there is), I would argue > that the pump IS the cutoff valve, and that adding a pilot operated > manual valve actually reduces safety by needlessly increasing > complexity and pilot workload. > > Marc, is quite right that the fuel system is a pain to work on when > the fuel can't be contained in the tank. But does this argue for a > pilot accessible fuel valve, or one directly at the tank exit? I > think it might be different issue from what I was first asking about, > but interesting nonetheless. > >>> Homepage: http://www.flyrotary.com/ >>> Archive: http://lancaironline.net/lists/flyrotary/List.html >> > >