Return-Path: Sender: (Marvin Kaye) To: lml Date: Mon, 13 May 2002 11:10:48 -0400 Message-ID: X-Original-Return-Path: Received: from smtprelay1.dc3.adelphia.net ([24.50.78.4] verified) by logan.com (CommuniGate Pro SMTP 4.0b1) with ESMTP id 1236167 for lml@lancaironline.net; Mon, 13 May 2002 09:27:37 -0400 Received: from worldwinds ([207.175.254.66]) by smtprelay1.dc3.adelphia.net (Netscape Messaging Server 4.15) with SMTP id GW1XCE00.8C6 for ; Mon, 13 May 2002 09:26:38 -0400 From: "Gary Casey" X-Original-To: "lancair list" Subject: engine reliability X-Original-Date: Mon, 13 May 2002 06:23:20 -0700 X-Original-Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) Importance: Normal X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2600.0000 <<2) Given the history and experience of brands C and L, I still maintain that it is inexcusable for out-of-the-box new Continental and Lycoming engines to break crankshafts, shear oil pump drives, and throw connecting rods. We should expect (and get) MUCH more. Certified engine reliability is NOT what it should be. 3) To expect that a NEWLY designed package will have the same reliability as a mature one is simply unrealistic. The prototype will never be as good as the later, more refined versions. Early production units would (should) not be as "good" as later production versions although the recent Continental and Lycoming experience causes one to review and question this assumption.>> Fred says it very well, but I would take some exceptions or maybe just add some comments. First, what degree of reliability are we looking for? I submit that it should be quite high - like an engine failure per more than 100,000 hours. And there are only two ways to determine reliability: By design and by experience. By experience, the L/C engines don't fare too well. A couple of broken cranks and rod bolts mess up the statistics pretty badly. By design they don't fare too well either - a rod bolt really shouldn't ever fail in a low-rpm engine unless something about it isn't designed right. And once a fix is in place the clock starts over - look at the Lycoming oil pumps - "now it is okay.....oops, no, I meant NOW it's okay.....well, try this..." and so on. Would I "expect" a newly designed engine to have equivalent reliability? That depends on the design as certainly there is no experience to fall back on. In this case experience seems to be a poor teacher as there are more failure modes lurking than there are "test" pilots willing to find them. The point is that if one wants to do something new it is not necessarily bad the result necessarily less reliable, but there are many, many design considerations that must be addressed. I once asked someone about his auto engine fuel system that I thought had built-in failure modes - the answer was "I've flown it for 100 hours with no problems" as though that were the proof. In fact, it was little more than anecdotal information; interesting, but not of much value. Gary Casey ES auto engine project