Return-Path: Received: from spdmgaac.compuserve.com ([149.174.206.136]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Sat, 19 Feb 2000 11:15:30 -0500 Received: (from mailgate@localhost) by spdmgaac.compuserve.com (8.9.3/8.9.3/SUN-1.9) id LAA06834 for lancair.list@olsusa.com; Sat, 19 Feb 2000 11:20:55 -0500 (EST) Date: Sat, 19 Feb 2000 11:19:29 -0500 From: RICHARD VAN GROUW <102077.3003@compuserve.com> Subject: Eagle 540 Sender: RICHARD VAN GROUW <102077.3003@compuserve.com> To: all Message-ID: <200002191120_MC2-99D9-285@compuserve.com> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I have finished the preliminary installation of the first Eagle 540 from American Engine in my Lancair IV-P. For those unfamiliar with this engine, I will give a little background. This is a scratch built aircraft engine based on a V-8 configuration rather than an auto engine conversion. The engine is water cooled with the radiator mounted in a belly nacelle(P-51 style) in the Lancair installation. The engine has dual redundant computers for control of all engine functions. There are dual fuel injectors for each cylinder and each cylinder has its own ignition coil. Ther are twin turbos and dual intercoolers. Displacement is 540 ci. The engine made over 800hp in the test cell but has been derated to 500hp for the LIV installation. With the dual turbos the engine will be able to make its rated power to >24,000 ft. This is a geared engine with helical gears and a torsional vibration isolator. For more details check the American Engine web site. The engine was run at low power settings for the fist several runs to check basic engine parameters and to check for leaks in the oil and cooling systems. I do not have my tach interfaced with the engine computer yet so I can not give specifics as to the exact power settings at which the engine was run. I hope to get the tach interface wired today and will be able to give more specific data in the future. Thus far the engine was run at idle which is reported as 1000 RPM on the engine and 560RPM on the prop based on test cell runs. It was run up to about 1/4 throttle for the first runs on the airframe. The engine is amazingly smooth at idle and through the power settings thus far. It is more suggestive of a turbine than a typical aircraft engine. I was also supprised that the noise was not as loud as I expected with the engine running at these low power settings( prior running of the engine has always been in the test cell with large mufflers conducting exhaust to the outside). I hope to keep you updated on the progress. This is an exciting time for me as I have been waiting for this engine for several years. It sure was good to finally see that prop spinning. Rick Van Grouw >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>