Return-Path: Received: from [65.33.166.167] (account ) by logan.com (CommuniGate Pro WebUser 4.0) with HTTP id 1850784 for ; Fri, 01 Nov 2002 19:34:40 -0500 From: "Marvin Kaye" Subject: Re: [LML] Re: More information on V-8 crash To: lml X-Mailer: CommuniGate Pro Web Mailer v.4.0 Date: Fri, 01 Nov 2002 19:34:40 -0500 Message-ID: In-Reply-To: <52548863F8A5D411B530005004759A93391661@QBERT> MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for George Braly : Gary, Help me understand something. I'm not trying to be critical. Assume NO accident happened. Did we have an experimental engine flying in a certified airframe on an experimental airworthiness certificate with 1) an engine that required 12 volts in order to operate; and 2) no way to monitor the 12 volt system; and 3) it was authorized for IFR flight; and 4) it was authorized for IFR flight at night? One of the reasons I want to know is because I could never in a million years get my Aircraft Certification Office and or MIDO and/or FISDO to approve those rather expansive "limitations" for flight with a new engine - - or even a certified engine with a minor modification - - much less doing that with an engine that required electricity and had no way to monitor the required 12 volt system. If this is being done in other regions, I need to know about it to get some leverage to open up the restrictions which we normally have to endure around here. Regards, George >>>> The current configuration has 2 pulleys and a vacuum pad. The buyer has the option of putting whatever (alternator, a/c compressor or vacuum pump) on any of these. Two batteries (I have twin 33AH SLAs) is standard. The point in this unfortunate event was the pilot had neither a voltmeter or ammeter to monitor the 14V charging system, as well as knowledge that the system was NOT charging. <<<<<