X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Wed, 09 Mar 2011 08:26:26 -0500 Message-ID: X-Original-Return-Path: Received: from elasmtp-galgo.atl.sa.earthlink.net ([209.86.89.61] verified) by logan.com (CommuniGate Pro SMTP 5.4c2) with ESMTP id 4900205 for lml@lancaironline.net; Tue, 08 Mar 2011 22:21:36 -0500 Received-SPF: none receiver=logan.com; client-ip=209.86.89.61; envelope-from=colyncase@earthlink.net DomainKey-Signature: a=rsa-sha1; q=dns; c=nofws; s=dk20050327; d=earthlink.net; b=g0TpMVcLqMoYIhIi+4ikrd4pvtK8lj11CxsEy/5h7noYf769876mjwv4+ekUUqXL; h=Received:Content-Type:Mime-Version:Subject:From:In-Reply-To:Date:Content-Transfer-Encoding:Message-Id:References:To:X-Mailer:X-ELNK-Trace:X-Originating-IP; Received: from [216.57.118.194] (helo=[192.168.1.107]) by elasmtp-galgo.atl.sa.earthlink.net with esmtpa (Exim 4.67) (envelope-from ) id 1Px9xM-0007nJ-N5 for lml@lancaironline.net; Tue, 08 Mar 2011 22:21:00 -0500 Content-Type: text/plain; charset=us-ascii Mime-Version: 1.0 (Apple Message framework v1082) Subject: Re: [LML] Re: LNC4 Observed Performance? From: Colyn Case In-Reply-To: X-Original-Date: Tue, 8 Mar 2011 22:21:00 -0500 Content-Transfer-Encoding: 7bit X-Original-Message-Id: <119C1514-7497-447D-A7DB-54CF13B10014@earthlink.net> References: X-Original-To: "Lancair Mailing List" X-Mailer: Apple Mail (2.1082) X-ELNK-Trace: 63d5d3452847f8b1d6dd28457998182d7e972de0d01da94017b5c9110d49932395f2390d2ba77bf3350badd9bab72f9c350badd9bab72f9c350badd9bab72f9c X-Originating-IP: 216.57.118.194 David can you post your climb rates all the way to fl250? On Mar 8, 2011, at 3:54 PM, Dr. Weinsweig wrote: > hi craig, > > although obviously biased i feel that the turbine ivp ie propjet is the > way to go. > > i see right around 300ktas from fl180(39 gph) to fl280(29gph) and > typically 32-33 gph at fl250 in my tks deiced propjet. with 146 gallons > usable i can comfortably plan for 900 nm and still have over an hour for > reserves. > > yes fuel burn is higher and range slightly less than a piston but when > you add climb/descent rates, short field advantages(due to power and > prop beta), perceived reliability, the smell of jet a, and the coolness > factor it is hard to beat! > > just my $.02 fwiw, > > david weinsweig > n750dw propjet 233 hrs- still for sale(need a family plane now) but > lovin' her > 304-633-5221 > weinsweigd@gmail.com > > >>>> cj@AwlBiz.com 03/02/2011 9:31 PM >>> > If this is posted elsewhere, please point me to the data. > > The Lancair site says a piston IV-P will do 330 mph (~286 KTAS) at > FL240. > I'd be interested in what speed and fuel-flow you guys see at > sustainable > power settings at various altitudes. > > Most of you flying LOP? I'm going to the APS class this Friday in > Ada. > > How much speed do you lose equipping with the thermal or TKS icing > products? > > Although probably beyond my budget, I'd also be interested in similar > data > for turbine-powered IVPs. > > My typical flight is 720 nm Oklahoma City to Phoenix, MEA 13000', > prevailing westerlies, 1-2 people and 50 lb stuff. The Mooney M20J > does > great on non-stop range and economy, but I'm evaluating options for > going > a lot faster, and preferably with at least inadvertent ice equipment. > Currently thinking Mooney Rocket, P-Baron, IV, IVP...? Thoughts on > appropriate planes would be welcomed. > > Craig > > > -- > For archives and unsub > http://mail.lancaironline.net:81/lists/lml/List.html > > -- > For archives and unsub http://mail.lancaironline.net:81/lists/lml/List.html