Return-Path: Received: from [65.33.165.45] (account marv@lancaironline.net HELO marvkaye.lancaironline.net) by logan.com (CommuniGate Pro SMTP 4.0b1) with ESMTP id 1251320 for lml@lancaironline.net; Wed, 29 May 2002 20:58:26 -0400 Message-Id: <5.1.0.14.2.20020529205941.04767c70@olsusa.com> X-Sender: marvkaye@lancaironline.net (Unverified) X-Mailer: QUALCOMM Windows Eudora Version 5.1 Date: Wed, 29 May 2002 21:01:18 -0400 To: lml@lancaironline.net From: Brent Regan (by way of marv@lancaironline.net) Subject: [Fwd: Re: Vacuum v. all electric] Mime-Version: 1.0 Content-Type: text/plain; charset="us-ascii"; format=flowed IMHO an all electric system is the hands down winner IF you replace the vacuum system with a standby alternator and battery. If you study the failure tree you will see that an all electric system with full backup and cross feed capability will provide a lot more options than an electrical and vacuum system together. This is due to the fact that you can't crossfeed electrons into a vacuum system and sucking on a wire does you no good either. "Hey Moe! No wonder water won't go through these pips. They's plugged wit wires!" Having said that, I did have the opportunity to design a vacuum system for a friends IV-P. He wanted a flight director so a vacuum system was a must have. I configured it with a vacuum regulator, filter and a small sonic venturi so that the system used filtered cabin air and discharged into the engine compartment. The advantage to this configuration was that when the vacuum pump failed (not IF) the cabin pressure would run the system. Free standby vacuum, works great. The bad news is that you have to watch for a vacuum flag when you transition to unpressurized flight in case the pump went T.U. in cruise. Regards Brent Regan