Return-Path: Received: from [24.25.9.101] (HELO ms-smtp-02-eri0.southeast.rr.com) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP id 577406 for flyrotary@lancaironline.net; Wed, 22 Dec 2004 18:38:39 -0500 Received-SPF: none receiver=logan.com; client-ip=24.25.9.101; envelope-from=eanderson@carolina.rr.com Received: from edward2 (cpe-069-132-111-212.carolina.rr.com [69.132.111.212]) by ms-smtp-02-eri0.southeast.rr.com (8.12.10/8.12.7) with SMTP id iBMNbv4S019614 for ; Wed, 22 Dec 2004 18:37:58 -0500 (EST) Message-ID: <005401c4e87f$03a6f320$2402a8c0@edward2> From: "Ed Anderson" To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: Fuel pump question. Date: Wed, 22 Dec 2004 18:36:08 -0500 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1106 X-MIMEOLE: Produced By Microsoft MimeOLE V6.00.2800.1106 X-Virus-Scanned: Symantec AntiVirus Scan Engine Joe, the principal reason for using both pumps on take-off and Landing is should one fail, the time it takes to recognize the problem, decided what has caused it and take corrective action (turn on the other pump), precious seconds can be lost. Which if you are close to the ground can made a crucial difference in the out come. I strongly recommend running both pumps for such critical phases of flight - you can turn one off when you reach a comfortable altitude (or have landed). Ed Anderson ----- Original Message ----- From: "Joe" To: "Rotary motors in aircraft" Sent: Wednesday, December 22, 2004 6:08 PM Subject: [FlyRotary] Re: Fuel pump question. > Dana, > I do not know of a reason to use both pumps at the same time. My thoughts > on this subject are directed to the electrical. If you use an single switch > it may have the effect of reducing redundancy. While redundancy exists for > the pump the wiring will not be fully redundant. The CB and wiring to the > common of your switch will serve both pumps and a failure in the CB, switch, > or lead in wiring will render both pumps inoperative. My current plans call > for 2 batteries, each pump, ECU supply, Coil supply etc. from each of the > batteries. > Joe > ----- Original Message ----- > From: "Dana Overall" > To: "Rotary motors in aircraft" > Sent: Tuesday, December 21, 2004 8:39 PM > Subject: [FlyRotary] Fuel pump question. > > > > Man am I ever going to expose my serious lack of electrical knowledge > > here:-) I'm planning on using a single pole double throw switch to > activate > > one or the other fuel pump, but not both. Is there ever any reason to > have > > both pumps on at the same time?? > > > > > > > > Dana Overall > > Richmond, KY i39 > > RV-7 slider, Imron black, "Black Magic" > > Finish kit > > 13B Rotary. Hangar flying my Dynon. > > http://rvflying.tripod.com > > http://rvflying.tripod.com/blackrudder.jpg > > do not archive > > > > > > > > >> Homepage: http://www.flyrotary.com/ > > >> Archive: http://lancaironline.net/lists/flyrotary/List.html > > > > > > >> Homepage: http://www.flyrotary.com/ > >> Archive: http://lancaironline.net/lists/flyrotary/List.html