Return-Path: Received: from dub-img-5.compuserve.com ([149.174.206.135]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Tue, 22 Dec 1998 12:29:49 -0500 Received: (from root@localhost) by dub-img-5.compuserve.com (8.8.6/8.8.6/2.17) id MAA11929 for lancair.list@olsusa.com; Tue, 22 Dec 1998 12:31:02 -0500 (EST) Date: Tue, 22 Dec 1998 12:30:05 -0500 From: Lynda Frantz Subject: Service Ceiling LC-2 Sender: Lynda Frantz To: "INTERNET:lancair.list@olsusa.com" Message-ID: <199812221230_MC2-6474-EFAD@compuserve.com> Mime-Version: 1.0 Content-Type: text/plain; charset=ISO-8859-1 Content-Disposition: inline X-Mailing-List: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> The service ceiling limit as quoted by Neico has nothing to do with the technical definition for service ceiling. I have talked to several LC-20 guys who have gotten their light craft up to FL240 and still climbing and Neico knows that the aircraft will go much higher than FL180. As I recall, (check with Neico) the 18,000 foot ceiling is due mostly to the flutter analysis test limits. As you go higher there is less flutter dampening and thus a lower critical flutter speed. Since the Lancair 320/360 is flutter limited, there is a maximum altitude airspeed combination at which this aircraft should be flown. Neico picked 18,000' and Vne. In other words, when flying above FL180, Neico does not make any claims. Sounds reasonable to me. And don't forget, if you fly at FL180 here in the USA it is only usable when the local barometric pressure is 29.92 or greater. So cruising IFR at FL180 is only available about half of the time. Jim Frantz Lancair Network News