Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.5.8) with ESMTP id 1156218 for rob@logan.com; Fri, 05 Apr 2002 21:02:06 -0500 Received: from siaag1ac.compuserve.com ([149.174.40.5]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71866U8000L800S0V35) with ESMTP id com for ; Fri, 5 Apr 2002 20:54:43 -0500 Received: (from mailgate@localhost) by siaag1ac.compuserve.com (8.9.3/8.9.3/SUN-1.12) id UAA28135 for lancair.list@olsusa.com; Fri, 5 Apr 2002 20:58:24 -0500 (EST) Date: Fri, 5 Apr 2002 20:58:08 -0500 From: James Frantz Subject: Glide Sender: James Frantz To: "INTERNET:lancair.list@olsusa.com" Message-ID: <200204052058_MC3-F8B2-4888@compuserve.com> MIME-Version: 1.0 Content-Transfer-Encoding: quoted-printable Content-Type: text/plain; charset=ISO-8859-1 Content-Disposition: inline X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> > I have heard that the results are very = different. I am sure that practicing this at idle is a good idea, but I = wouldn't bank on that observed ratio with the engine stopped.< I agree. I like to think in terms of miles of glide per 1000 feet of altitude loss. = If my engine ever quits, I am going = to find a place to land within 2 miles for every 1000' AGL assuming no wind and the gear and flaps up. = That is only a 10.5:1 glide ratio which I = think is more realistic in an engine out emergency for a 360. With gear and flaps down and the prop in fine pitch, figure about half the above. James B. Frantz >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://members.olsusa.com/mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please remember that purchases from the Builders' Bookstore assist with the management of the LML. Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>