Return-Path: Sender: (Marvin Kaye) To: lml Date: Thu, 30 May 2002 20:25:31 -0400 Message-ID: X-Original-Return-Path: Received: from imo-m01.mx.aol.com ([64.12.136.4] verified) by logan.com (CommuniGate Pro SMTP 4.0b1) with ESMTP id 1252225 for lml@lancaironline.net; Thu, 30 May 2002 18:40:11 -0400 Received: from RWolf99@aol.com by imo-m01.mx.aol.com (mail_out_v32.5.) id q.4c.c2faded (3972) for ; Thu, 30 May 2002 18:40:03 -0400 (EDT) From: RWolf99@aol.com X-Original-Message-ID: <4c.c2faded.2a280442@aol.com> X-Original-Date: Thu, 30 May 2002 18:40:02 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 Been awhile since I posted anything, but I've just had my computer guru tell me how to decode those freakin' MIME files and I'm getting caught up with the list... I disagree with the group consensus that all-electric is the only way to go. Seems to me a lot of airplanes fly pretty well with the traditional vacuum AI & DG and the electric turn coordinator. As I recall, the likelihood of crashing due to a failed vacuum system is far, far less than due to running out of gas or continued VFR into IMC. Doesn't runnign out of gas cause something like 40% of all crashes? Continued VFR into IMC another 40%? How many crashes are caused by a vacuum system crapping out? Some, but not many. I suppose you hard-IFR-all-the-time guys could benefit from the extra complexity of an all-electric system, but now you've got probably ten pounds of extra crap and several thousand dollars of extra cost that you drag around with you all the time. Plus, you haven't yet addressed the issue of the gyro itself failing -- just it's power source. I'm a fairly inexperienced IFR pilot -- I may punch through marine layers, but if it's really raining I stay on the ground. I couldn't care less about Stormscopes and Strikefinders since in this fiberglass airplane with my limited IFR experience I have no business trying to thread my way through thunderstorm cells or heavy rain showers. This is not to say that I'll never be in the soup, but the percentage of the time I'll be there is going to be pretty small. So maybe I'm burying my head in the sand by ignoring the likelihood of vacuum failure, but maybe not. In my Cessna the vacuum gauge was way over on the other side of the airplane, where I never looked at it. In my 360 it will be right next to the AI where it's plainly visible. In addition, I'll have a low vacuum switch tied into Jim Frantz's annunciator system. And let's not forget my resolution to practice partial panel on a regular basis. It's all about risk management. My risks of perishing due to a vacuum failure are low since I'm not IFR that much and I'll have warning systems to alert me to the vacuum failure. My risks of not finishing the airplane due to extra cost and time to install a dual-redundant electrical system and gyros which cost 4-5 times as much as the vacuum ones are significantly higher. If I were to add weight and dollars to the project, I'd make the fuel system bulletproof -- not the IFR instrumentation. But I think I've already done that by keeping the relatively simple header tank installation. Perhaps as I get more IFR experience and begin to feel comfortable in hard IFR, plus after I've paid off all the loans, I'll retrofit a dual electric system and the high cost electric gyros. But for now, I'll stay the same as 99 percent of the aviation fleet with the traditional setup, and take my chances. - Rob Wolf