X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [66.37.197.101] (HELO o1.xlccorp.com) by logan.com (CommuniGate Pro SMTP 5.1.2) with SMTP id 1598980 for flyrotary@lancaironline.net; Fri, 24 Nov 2006 08:45:11 -0500 Received-SPF: none receiver=logan.com; client-ip=66.37.197.101; envelope-from=bbradburry@allvantage.com Received: (qmail 18524 invoked from network); 24 Nov 2006 13:44:47 -0000 Received: from dialup-4.235.39.125.dial1.orlando1.level3.net (HELO ?4.235.39.125?) (bbradburry@4.235.39.125) by o1.xlccorp.com with SMTP; 24 Nov 2006 13:44:47 -0000 Message-ID: <4566F776.2010208@allvantage.com> Date: Fri, 24 Nov 2006 08:45:26 -0500 From: Bill Bradburry Reply-To: bbradburry@allvantage.com User-Agent: Thunderbird 1.5.0.8 (Windows/20061025) MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Z-19 questions References: In-Reply-To: Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit OK, This is my fall back position. I have posed this question on the Aerolectric list for a couple of days and no answer. (although the email did get caught up in an embarrasing event!) 90% of you guys have already wired your planes and followed Bob N's advice, so how did you do the redundancy on the fuel pumps, coils, and injectors? from the AE list: "I am installing a fuel injected Mazda rotary engine and trying to follow the Z-19 guidelines for dual battery, single alternator. Looking at the engine primary and secondary circuit, I need to install a primary and secondary fuel pump, plus I want to power the coils and the injectors off of the battery buss. How should I do this? I suppose I could take the fuel pump diode output and switch it to either of the two fuel pumps??? What about the coils and injectors? Should I set up similar circuits for them, or is there a better way to reduce parts??? I would appreciate any guidance you guys could give me. Thanks and Happy Thanksgiving! Bill B