Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.4.5) with ESMTP id 773395 for rob@logan.com; Thu, 03 May 2001 22:03:58 -0400 Received: from qbert.gami.com ([38.193.29.253]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71175U5500L550S0V35) with ESMTP id com for ; Thu, 3 May 2001 21:19:03 -0400 Received: by QBERT with Internet Mail Service (5.5.2650.21) id ; Thu, 3 May 2001 20:26:55 -0500 Message-ID: <52548863F8A5D411B530005004759A930126C5@QBERT> From: George Braly To: "'lancair.list@olsusa.com'" Cc: "Timothy C. Roehl" Subject: RE: transition:ROP to LOP Date: Thu, 3 May 2001 20:26:54 -0500 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Tony, I did not intend to suggest that all turbo'd engines could or should be operated at WOT at cruise. I think I said: "On the normally aspirated engines, I recommend that all takeoff, climb and cruise operations be done with wide open throttle... (WOT) even at cruise at 1000' MSL. However, one can modulate the horsepower by using the red knob and the blue knob." Someplace else, I probably also said that I operate my 8.5:1 compression ration turbo-normalized IO-550 at WOT (which is 30"). Thanks for making it clear that the boosted engines need to come off the throttle somewhat for continuous cruise. Having said that, I have operated a number of TSIO-520 and TSIO-550 engines at 32 and 33" and sometimes 34" while well lean of peak. I have never seen them "complain" (that's a good term, by the way... I like it) about it, as long as they are well lean of peak. During FAA flight testing for the certification of the turboGAMIjector fuel injectors, we were required to do a climb cooling test with my IO-550 (8.5:1 CR) set up from the "normal" 30" all the way to 35" of MP. We took it to 25,000'. It ran just fine lean of peak at all manifold pressures up to 35". On the 8.5:1 engines, one ought not to try that except under those special test and instrumentation conditions. Looking at the data, I see no reason that the TSIO-520/550 engines with 7.5:1 compression ratios will not operate just fine up to about 33", provided they are operating smoothly lean of peak and the CHTs are well under control. However, if you are sensing that the engine is "complaining" above 30", then I would like to get a chance to go along and see if I can figure out what is going on. Drop in and see us sometime! Regards, George Braly >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>