X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Fri, 05 Aug 2011 10:37:36 -0400 Message-ID: X-Original-Return-Path: Received: from nm11-vm1.bullet.mail.ne1.yahoo.com ([98.138.91.40] verified) by logan.com (CommuniGate Pro SMTP 5.4.1) with SMTP id 5082794 for lml@lancaironline.net; Fri, 05 Aug 2011 08:49:00 -0400 Received-SPF: none receiver=logan.com; client-ip=98.138.91.40; envelope-from=casey.gary@yahoo.com Received: from [98.138.90.56] by nm11.bullet.mail.ne1.yahoo.com with NNFMP; 05 Aug 2011 12:48:25 -0000 Received: from [98.138.89.169] by tm9.bullet.mail.ne1.yahoo.com with NNFMP; 05 Aug 2011 12:48:25 -0000 Received: from [127.0.0.1] by omp1025.mail.ne1.yahoo.com with NNFMP; 05 Aug 2011 12:48:25 -0000 X-Yahoo-Newman-Property: ymail-3 X-Yahoo-Newman-Id: 184642.2063.bm@omp1025.mail.ne1.yahoo.com Received: (qmail 14851 invoked by uid 60001); 5 Aug 2011 12:48:25 -0000 DomainKey-Signature:a=rsa-sha1; q=dns; c=nofws; s=s1024; d=yahoo.com; h=X-YMail-OSG:Received:X-Mailer:References:Message-ID:Date:From:Reply-To:Subject:To:In-Reply-To:MIME-Version:Content-Type; b=vmQ0m/po4Tc8TS+ac2PRPCVKWbJ64jTxf3VLsyoI8OYQWTLcE2aKkd9LFNEsI8SYnQoFmdO6Akh1VFw9vpWeq9k8/lLwKoTixK9D8o4DtBv13chgdIqhQ/zhMv1/HuESn+m/5jOjf9JDVszvf3ybEvDv6ZXhIJg9EajKOzrUR08=; X-YMail-OSG: FvQb4hEVM1mlkTDd21Oys7rlvAhxinZ6Wgfd6LavoOmqct3 dmehUV8ssANmx6OENc_DQ.ckt3L2hAo7hJc5g2pRBuuIBuGCP8.RUJ5bWXPR eg0TEuZ5ZH5eqzuKSmjsmIoW3A32EtVcehTkFyV.4HtTxlb1dc5aCElqTo5Z EY7gaqUmVO1K4o3.UsLJAGKmtvLrk4o70dlC18yme.R13OjLpH4kMSvp1xz4 WiOciWuGKa3T6Bma8BFhLgm64xVgJXVEZEHzhX5JeoB811WljuPE8JRnKy4I Rf91ApuX1H9kvJQlY2eYsHuE4v3zrx8foQ4zETH8q7Ipk.DOfhO7yrldJSnc jsP9t5B7fft0_MRn4gly1NII1QosobrerbrETfkb0Fg-- Received: from [97.122.183.58] by web125602.mail.ne1.yahoo.com via HTTP; Fri, 05 Aug 2011 05:48:24 PDT X-Mailer: YahooMailWebService/0.8.113.313619 References: X-Original-Message-ID: <1312548504.11577.YahooMailNeo@web125602.mail.ne1.yahoo.com> X-Original-Date: Fri, 5 Aug 2011 05:48:24 -0700 (PDT) From: Gary Casey Reply-To: Gary Casey Subject: Re: Re-doing my panel - carefully thinking through failures X-Original-To: Lancair Mailing List In-Reply-To: MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="0-1604840668-1312548504=:11577" --0-1604840668-1312548504=:11577 Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable I also concur with Brent, but I arrived at perhaps a diametrically opposite= conclusion from Fred's. =A0I also have dual Chelton screens, but only have= one battery and one alternator. =A0The backup is a vacuum-powered 6-pack i= n a standard configuration on the right side. =A0True, it isn't in the "nor= mal scan" as Brent would suggest, but it is close enough to fly by it. =A0T= here are no "manual work-arounds" as Fred has. =A0The idea is that the weak= link in the chain (the pilot) will probably turn to mush in an emergency, = so let's reduce his workload, not ask him to do more. =A0If there is an ele= ctrical failure, the idea is to get on the ground, if necessary with the ha= ndheld radio, and fix it there. =A0Just my thoughts.=0AGary=0A=0APreviously= from Fred:=0ABrent=A0has written much on this topic including "In my "Glaz= ed and Confused" presentation on "Glass Cockpits" I say that flying an airc= raft with a non-certified, non TSO'ed glass standby (Dynon et al) is like j= umping out of an airplane with only your main parachute and your standby pl= an is the fact you are wearing real soft socks."=0A=A0=0AI concur.=A0=0A=A0= =0AWhen I was young and stupid (not long ago) I had thoughts of long overwa= ter (think trans-Pacific) flights.=A0 I also have experience with failure m= odes assessment analysis (FMEA) which frequently shows up failure modes eas= ily over looked.=A0 After reviewing various electrical and instrument confi= gurations I arrived at a system design which is shown in simplified form in= the attached sketch.=A0 It consists of two alternators, two batteries, fou= r busses, and a lot of opportunities for cross tie.=A0 I use dual Chelton s= creens, with PFD off the essential buss (many sources of power), the MFD of= f of the avionics bus (which has many sources of power), and back up electr= ic attitude=A0 indicator (on essential buss), turn and bank (essential buss= ) and air speed and altitude indicators.=0A=A0=0AYou show me the failure an= d I can show you the automated or manual work around. --0-1604840668-1312548504=:11577 Content-Type: text/html; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable
I also concur = with Brent, but I arrived at perhaps a diametrically opposite conclusion fr= om Fred's.  I also have dual Chelton screens, but only have one batter= y and one alternator.  The backup is a vacuum-powered 6-pack in a stan= dard configuration on the right side.  True, it isn't in the "normal s= can" as Brent would suggest, but it is close enough to fly by it.  The= re are no "manual work-arounds" as Fred has.  The idea is that the wea= k link in the chain (the pilot) will probably turn to mush in an emergency,= so let's reduce his workload, not ask him to do more.  If there is an= electrical failure, the idea is to get on the ground, if necessary with th= e handheld radio, and fix it there.  Just my thoughts.
Gary

Previously from Fred:
Brent has written much on this topic including "In my "Glazed = and Confused" presentation on "Glass Cockpits" I say that flying an aircraf= t with a non-certified, non TSO'ed glass standby (Dynon et al) is like jump= ing out of an airplane with only your main parachute and your standby plan = is the fact you are wearing real soft socks."
 
I = concur. 
 
When I was young and stupid (not l= ong ago) I had thoughts of long overwater (think trans-Pacific) flights.&nb= sp; I also have experience with failure modes assessment analysis (FMEA) wh= ich frequently shows up failure modes easily over looked.  After revie= wing various electrical and instrument configurations I arrived at a system= design which is shown in simplified form in the attached sketch.  It = consists of two alternators, two batteries, four busses, and a lot of opportunities for cross tie.  I use dual Chelton screens, with PFD= off the essential buss (many sources of power), the MFD off of the avionic= s bus (which has many sources of power), and back up electric attitude = ; indicator (on essential buss), turn and bank (essential buss) and air spe= ed and altitude indicators.
 
You show me the fail= ure and I can show you the automated or manual work around.


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