Return-Path: Received: from teapot06.domain1.bigpond.com ([139.134.5.237]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with SMTP id com for ; Mon, 9 Oct 2000 07:54:57 -0400 Received: from localhost (localhost [127.0.0.1]) by teapot06.domain1.bigpond.com (NTMail 3.02.13) with ESMTP id fa496085 for ; Mon, 9 Oct 2000 21:47:57 +1000 Received: from MDIP-A-005-pool-233.tmns.net.au ([139.134.178.233]) by mail1.bigpond.com (Claudes-Tidy-MailRouter V2.9c 1/4511972); 09 Oct 2000 21:47:55 Message-ID: <000a01c031e6$e524b0c0$e9b2868b@oemcomputer> From: "Mr Gary Burns" To: Subject: Fw: Walter 601D powered Lancair IVP Date: Mon, 9 Oct 2000 21:48:06 +1000 X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> ----- Original Message ----- From: Mr Gary Burns To: lancair.list@olsusa.com Cc: Lance Neibauer ; Frank Fry Sent: Monday, 9 October 2000 11:22 Subject: Walter 601D powered Lancair IVP Here is an update on some of the test flying results of Frank Fry's Lancair Turbine.Every one was keen to find out how it goes at altitude so here are some preliminary figures. The climb to 25,000 feet took exactly six & one half minutes initially with 85% torque & 1850 RPM. At top of climb there was an abundance of power to go much higher.58% torque was still available at this altitude. The fuel flow at this levl was 109 litres per hour or by my calculation 28.794752 US Gallons per hour.This engine has 1500 hours since last overhaul & is due for a compressor wash , so the fuel flow should come down, especially if flown higher. The indicated airspeed of 195 knots for a true airspeed of about 295 knots was disappointing but we attribute this low speed to the inefficient propellor design. The prop is off the LET 410 & has 4 inches cut off it for ground clearance purposes. The Let is an old design with a cruise speed around 180 to 200 knots so it is a big ask to expect the prop to be efficient at these higher speeds. Frank will attempt to source the Avia 84" higher performance blades when they become available. The ideal prop would be a Hartzell purpose built & at Oshkosh this year they mentioned they have a blade design in mind for the Walter. If more builders went down the path of the turbine, I am sure Hartzell would expedite the building of this prop. I will report more on the progress of this exciting aircraft as test results come to hand. Regards Gary Burns >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>