Return-Path: Received: from SMTP02.INFOAVE.NET ([165.166.0.27] verified) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP id 577413 for flyrotary@lancaironline.net; Wed, 22 Dec 2004 18:44:12 -0500 Received-SPF: none receiver=logan.com; client-ip=165.166.0.27; envelope-from=jewen@comporium.net Received: from home1 ([199.222.166.174]) by SMTP00.InfoAve.Net (PMDF V6.2-X31 #30986) with SMTP id <01LIPJMM8J909BVQTP@SMTP00.InfoAve.Net> for flyrotary@lancaironline.net; Wed, 22 Dec 2004 18:43:33 -0500 (EST) Date: Wed, 22 Dec 2004 18:42:19 -0500 From: Joe Subject: Re: [FlyRotary] Re: Fuel pump question. To: Rotary motors in aircraft Message-id: <018601c4e87f$e07c7540$6432a8c0@home1> MIME-version: 1.0 X-MIMEOLE: Produced By Microsoft MimeOLE V6.00.2800.1441 X-Mailer: Microsoft Outlook Express 6.00.2800.1437 Content-type: text/plain; charset=iso-8859-1 Content-transfer-encoding: 7bit X-Priority: 3 X-MSMail-priority: Normal References: Ed, Thanks, just after I hit the send button I thought of the reason for both to be on. Joe. ----- Original Message ----- From: "Ed Anderson" To: "Rotary motors in aircraft" Sent: Wednesday, December 22, 2004 6:36 PM Subject: [FlyRotary] Re: Fuel pump question. > 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 > > > > >> Homepage: http://www.flyrotary.com/ > >> Archive: http://lancaironline.net/lists/flyrotary/List.html >