Return-Path: Received: from hotmail.com ([216.33.241.97]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Wed, 25 Oct 2000 19:24:18 -0400 Received: from mail pickup service by hotmail.com with Microsoft SMTPSVC; Wed, 25 Oct 2000 16:31:16 -0700 Received: from 63.67.151.2 by lw8fd.law8.hotmail.msn.com with HTTP; Wed, 25 Oct 2000 23:31:16 GMT From: "Eric Parlow" To: lancair.list@olsusa.com Subject: Re: To Eric Parlow via the LML, re engines for the ES Date: Wed, 25 Oct 2000 23:31:16 GMT Message-ID: X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Jim, Q--: Can the turbo'ed version of the IO-360 get by with 80/87 or the forthcoming 82UL? A-- No, All TSIO-360 engines require 100LL. Turbo-normalized engines will make the equivalent power at altitude but the intake air temperature created by the turbocharger reduces detonation margin. The IO-360-B engine is only 360 certified for use with 80/87. It is 180 bhp @ 2700 rpm. It has 6.5:1 compression. Q-- If so, I would think this would be an attractive alternate engine for the ES. At altitude with the turbo-normalization, my guess is that the performance numbers would not be far off those for the Super ES with the IO-550. A--TSIO-360-MB would be the engine of choice. It is 220 bhp @ 2600 rpm with a MAP of 38 inHg and a service ceiling of 19,000 ft. The IO-550-N only makes 220 bhp below 10,000 ft. The TSIO-360-MB weights 354 lb vs an IO-550-N at 428 lb. Q--Orrin seems to have a nice turbo 360 setup in his two-seater. Comments? A--Yes, but it's the wrong color! ERic-- >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>