Return-Path: Received: from smtp11.bellglobal.com ([204.101.251.53]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Fri, 19 Nov 1999 10:54:33 -0500 Received: from default (ppp134.on.bellglobal.com [206.172.245.134]) by smtp11.bellglobal.com (8.8.5/8.8.5) with SMTP id LAA07310 for ; Fri, 19 Nov 1999 11:03:12 -0500 (EST) Message-ID: <02b301bf32a6$9f27aa40$16f5acce@default> From: "Ian B. Crowe" To: "Marvin Kaye" Subject: Fuel pump installation Date: Fri, 19 Nov 1999 10:55:40 -0500 Organization: Corvi Trade Consultants Inc X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I have no definitive words of wisdom for the positioning of the fuel pump. I notice there has been no reply to the post requesting help on this so here goes my "Two cents worth" Canadian. I am also going to put the fuel pump on the rear side of the firewall. So at least I am a true believer! 1. I feel that it will be away from the under cowling heat which has to be beneficial for the fuel and will help it to not to vaporise. Also the electrics of the pump will love you for keeping them cool. 2. It is a lot easier to push vaporised fuel than to pull it . With the pump in the cockpit you will always have relatively cool fuel to suck compared with the fuel on the other side of the fire wall. 3. If it leaks or even weeps you will smell it at once and hopefully be able to deal with it before it becomes a major problem. The opposite is true if it is under the cowling and the heat source is always there in flight. Also under the cowling means that you never get to see it unless the cowling is off or the leak is heavy. Remember that you do not need the pump running all the time, landing, take off, climb out and at tank change time should do it. The rest of the time the engine driven pump will be running the system and the lines will be under suction. 4. I am taking good care in the installation of the pipework to and from the pump, using the same level of care as I have done with the fuel changeover valve. Again this is cockpit located. Proper clamping to avoid vibration is mandatory. I shall pressure test the whole system with shop air at 90psi. Please bear in mind that I have no professional qualifications to advise you and the foregoing is my attempt to satisfy good practice. Also I am a long way from the reach of your convuluted tort system!!!!!!!! Got to get the obligatory hit in about the legal profession. Seriously though that is my considered opinion and I would love it if one of our better qualified brethren could put forward a counter proposal. Hate to rip out all that lovely bent pipe but there it is. (All my lines are solid 3/8" aluminum) Kind regards Ian Crowe >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>