Return-Path: Sender: (Marvin Kaye) To: lml Date: Fri, 17 Oct 2003 12:52:11 -0400 Message-ID: X-Original-Return-Path: Received: from apollo.email.starband.net ([148.78.247.132] verified) by logan.com (CommuniGate Pro SMTP 4.1.5) with ESMTP id 2640501 for lml@lancaironline.net; Fri, 17 Oct 2003 11:15:05 -0400 Received: from regandesigns.com (vsat-148-63-101-227.c002.t7.mrt.starband.net [148.63.101.227]) by apollo.email.starband.net (8.12.9/8.12.9) with ESMTP id h9HFIO8H003709 for ; Fri, 17 Oct 2003 11:18:26 -0400 X-Original-Message-ID: <3F900772.9060102@regandesigns.com> Disposition-Notification-To: Brent Regan X-Original-Date: Fri, 17 Oct 2003 08:14:58 -0700 From: Brent Regan User-Agent: Mozilla/5.0 (Windows; U; Windows NT 5.1; en-US; rv:1.0.2) Gecko/20021120 Netscape/7.01 X-Accept-Language: en-us, en MIME-Version: 1.0 X-Original-To: Lancair Subject: R: Of Men and EFIS Content-Type: text/plain; charset=us-ascii; format=flowed Content-Transfer-Encoding: 7bit Shannnon writes: <> They don't. There is a difference between "Cant be on during cranking" and "we do not recommend having it on during cranking". As an engineer I am interested in the equipment's capabilities but the manufacturers recommendations may follow convention and be more conservative. Im my 28 volt airplane there is no avionics buss switch so all my avionics, including the EFIS, are on during cranking. If I had built a 12 volt airplane then I probably would have included an avionics switch to reduce the load on the battery during cranking. Experience and testing show that the EFIS will ride through or reboot and function properly after a brown out. YOU are obliged to follow the manufacturers recommendations, unless you are an idiot like me. Regards Brent Regan