X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Wed, 01 Jun 2011 11:50:42 -0400 Message-ID: X-Original-Return-Path: Received: from imr-db02.mx.aol.com ([205.188.91.96] verified) by logan.com (CommuniGate Pro SMTP 5.4c3j) with ESMTP id 5000294 for lml@lancaironline.net; Wed, 01 Jun 2011 08:34:32 -0400 Received-SPF: pass receiver=logan.com; client-ip=205.188.91.96; envelope-from=vtailjeff@aol.com Received: from mtaout-ma06.r1000.mx.aol.com (mtaout-ma06.r1000.mx.aol.com [172.29.41.6]) by imr-db02.mx.aol.com (8.14.1/8.14.1) with ESMTP id p51CXlE5004485 for ; Wed, 1 Jun 2011 08:33:47 -0400 Received: from [10.77.53.238] (unknown [166.205.9.25]) (using TLSv1 with cipher AES128-SHA (128/128 bits)) (No client certificate requested) by mtaout-ma06.r1000.mx.aol.com (MUA/Third Party Client Interface) with ESMTPSA id C7169E00008D; Wed, 1 Jun 2011 08:33:45 -0400 (EDT) References: In-Reply-To: Mime-Version: 1.0 (iPad Mail 8C148) Content-Type: text/plain; charset=us-ascii X-Original-Message-Id: <9D4E2691-E236-42DC-BA0B-8213366B972A@aol.com> Content-Transfer-Encoding: quoted-printable X-Mailer: iPad Mail (8C148) From: vtailjeff@aol.com Subject: Re: [LML] Re: L-IV Choice of Engine X-Original-Date: Wed, 1 Jun 2011 06:33:40 -0600 X-Original-To: Lancair Mailing List x-aol-global-disposition: G X-AOL-SCOLL-SCORE: 0:2:414892320:93952408 X-AOL-SCOLL-URL_COUNT: 0 x-aol-sid: 3039ac1d29064de631a9321a X-AOL-IP: 166.205.9.25 Ted, I think this group will offer some well thought "but what if?" comments to y= our project. Many are worth consideration. Best of luck with it. Jeff Edwards Sent from my iPad On Jun 1, 2011, at 5:42 AM, Hamid Wasti wrote: > Ted Noel wrote: >> Your comments below are part of what drives me nuts in this conversation.= A fuel line failure is NOT an engine issue. It is a systems issue that appl= ies to every aircraft that ever flew (except electrics). Thus, using it as a= condemnation of a one-off application is not germane to the topic. > Actually, it is exactly the issue and your not recognizing it as such make= s me worry about your grasp of the problem. >=20 > The fuel system on every aircraft that ever flew was designed, tested and v= alidated over years and decades and that validation paid for in blood and li= ves. If you want to take advantage of that validation, fly one of those syst= ems. Otherwise the one-of fuel system in your one-of implementation is as un= tested as the engine it is feeding. You trivialize it and other systems at t= he peril of your life. >=20 > When you buy a Lycoming engine for your airplane or a Ford engine for your= car, someone has done all the engineering including the system level engine= ering. Even though the engine does not come with a fuel line or electric cab= les, the knowledge of how to make those connections comes with the engine. W= hen you install the engine, you are implementing an existing and validated d= esign. You are not designing something new. >=20 > When you do a one-of design, you have to design those systems from scratch= . You can learn from what Lycoming or Ford did, but it is still a new design= and subject to errors, oversights and other mistakes. The more things you a= re designing in an implementation, the higher the probability that errors wi= ll be present in the final system and that one of these errors could start a= catastrophic chain reaction. >=20 > You have talked a lot about your engine. What is your operational history?= How many hundred hours do you fly each year and how many hundred hours have= you flown? What are your operational results for fuel consumption, temperat= ures and performance? >=20 > Regards, >=20 > Hamid >=20 >=20 > -- > For archives and unsub http://mail.lancaironline.net:81/lists/lml/List.htm= l