X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sat, 09 Jul 2011 11:34:42 -0400 Message-ID: X-Original-Return-Path: Received: from mail-wy0-f180.google.com ([74.125.82.180] verified) by logan.com (CommuniGate Pro SMTP 5.4.0) with ESMTPS id 5046058 for lml@lancaironline.net; Fri, 08 Jul 2011 15:18:14 -0400 Received-SPF: pass receiver=logan.com; client-ip=74.125.82.180; envelope-from=keith.smith@gmail.com Received: by wye20 with SMTP id 20so1568837wye.25 for ; Fri, 08 Jul 2011 12:17:36 -0700 (PDT) MIME-Version: 1.0 Received: by 10.227.157.134 with SMTP id b6mr2142963wbx.59.1310152656165; Fri, 08 Jul 2011 12:17:36 -0700 (PDT) Received: by 10.227.68.196 with HTTP; Fri, 8 Jul 2011 12:17:36 -0700 (PDT) In-Reply-To: References: X-Original-Date: Fri, 8 Jul 2011 15:17:36 -0400 X-Original-Message-ID: Subject: Re: [LML] Re: n23ph From: Keith Smith X-Original-To: Lancair Mailing List Content-Type: multipart/alternative; boundary=0016364d2a99ac1cf804a793af90 --0016364d2a99ac1cf804a793af90 Content-Type: text/plain; charset=ISO-8859-1 My simulated engine out testing has shown 550-600fpm at 100kias with 3/4 fuel and just me in the airplane. I had a real engine out up at 10k a while ago. Descent rate at 100kias up at 10k was right around 1000fpm. SOME of that could be attributed to the higher TAS. SOME of it could be attributed to the higher weight. SOME of it could be attributed to me flying slightly faster than 100kias. The rest, I assume, is the difference between idle thrust and a zero combustion excursion. Keith --0016364d2a99ac1cf804a793af90 Content-Type: text/html; charset=ISO-8859-1 Content-Transfer-Encoding: quoted-printable My simulated engine out testing has shown 550-600fpm at 100kias with 3/4 fu= el and just me in the airplane.

I had a real engine out up at 10k a = while ago.=A0 Descent rate at 100kias up at 10k was right around 1000fpm.= =A0 SOME of that could be attributed to the higher TAS. SOME of it could be= attributed to the higher weight. SOME of it could be attributed to me flyi= ng slightly faster than 100kias. The rest, I assume, is the difference betw= een idle thrust and a zero combustion excursion.

Keith
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