Return-Path: Received: from ares.flash.net ([209.30.0.41]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Wed, 16 Jun 1999 17:12:03 -0400 Received: from flash.net (209-30-241-57.flash.net [209.30.241.57]) by ares.flash.net (8.9.3/8.9.3) with ESMTP id QAA11642; Wed, 16 Jun 1999 16:14:57 -0500 (CDT) Message-ID: <37681036.3EBFD15C@flash.net> Date: Wed, 16 Jun 1999 15:59:34 -0500 From: Ken Harwood To: "lancair.list@olsusa.com" Subject: RE: 360 vs 320 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Bigger is Better!! Remember the extra weight is all going into horsepower. You can expect much better climb performance on a hot day/heavy airplane combination with a bigger engine. I installed (shoe horned) a Lycoming IO-360A engine into my Lancair and although it required major modifications to the cowling, it sure performs nicely; especially since it has 10:1 pistons, etc. Lycon of Visalia says it produces 241 hp but a more realistic figure based on how much hp you get from increasing compression, fuel flow data, and flow balancing would probably be around 220 hp - about 10% increase over the stock 200 hp engine. Cruise speed is about 210 kts. I get consistent cruise speeds in excess of 200 kts at any altitude up to about 13,000 ft. I typically flight plan for 200 kts and if I find I have a head wind, I push in a little more throttle or RPM and make some of that head wind go away. I believe these cruise speeds are about 15 kts above most Lancair 320's with constant speed props. Another nice trick is to put a ported and flow balanced Lycoming 0-320 into a Lancair 235. Steve King has one of those babies and it really performs nicely. Ken Harwood, N15KH >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html