Return-Path: Sender: (Marvin Kaye) To: lml Date: Fri, 31 May 2002 16:34:38 -0400 Message-ID: X-Original-Return-Path: Received: from imo-r07.mx.aol.com ([152.163.225.103] verified) by logan.com (CommuniGate Pro SMTP 4.0b1) with ESMTP id 1252998 for lml@lancaironline.net; Fri, 31 May 2002 15:11:41 -0400 Received: from RWolf99@aol.com by imo-r07.mx.aol.com (mail_out_v32.5.) id q.97.2858cba8 (3968) for ; Fri, 31 May 2002 15:11:33 -0400 (EDT) From: RWolf99@aol.com X-Original-Message-ID: <97.2858cba8.2a2924e4@aol.com> X-Original-Date: Fri, 31 May 2002 15:11:32 EDT Subject: Re: Vacuum v all electric X-Original-To: lml@lancaironline.net MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Mailer: AOL 5.0 for Windows sub 108 I thought I'd get a response to my position that the traditional vacuum AI & DG with an electric TC is good enough for me, and the list has not let me down.... Jeff, I have no issue with your claim that an all-electric gyro system eliminates gyro failures due to loss of vacuum. I will go a step further and assert that, if properly implemented (and that's a key point), a redundant electric power system can be made far more reliable than a vacuum system, which we should all know will fail someday if not changed prophylactically beforehand. My guesstimate for MTBF (mean time between failures) for the vacuum system is something around 500 hours, based on anecdotal information in the aviation publications. I will point out that Airborne now has a wear indicator on their new vacuum pumps, although I don't know whether the dry vacuum pumps wear down or fracture for other reasons. In any event, electrics should be more reliable IF properly implemented. However, history has shown that the likelihood of crashing due to a vacuum failure is tiny compared to other causes, and that was my main point. Here's another example -- how many people die in midairs? Probably more than due to vacuum failures. How many Lancairs have TCAS? Not many. Wouldn't you rather put your extra money and weight in a TCAS system than another battery and $1500-per-each gyros? Statistically, that's the wiser choice (and no, I can't afford that either, but wish that I could). My claim was only that loss of control due to vacuum failures represents a tiny fraction of the fatal accidents experienced in the 50 years or so since the configuration became a de facto standard. Further, my supposition is that the real problem is not noticing that the vacuum is gone until you're in an unusual attitude, and that most of us have the skills to fly partial panel IF we are warned that the vacuum is gone and we cover up the AI and DG before they spin down (hence the warning system I'm installing). I recognize that my choice is not the right one for everyone, and actually would prefer that the antediluvian vacuum system would disappear. Too bad I just can't afford it. That doesn't mean that my airplane shouldn't ever poke it's nose into a cloud, though. Thanks for your comments, on this and other issues. - Rob Wolf