Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.5.1) with ESMTP id 998720 for rob@logan.com; Thu, 27 Dec 2001 13:58:02 -0500 Received: from dewey.Cadwell.cadwell.com ([208.26.246.18]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71866U8000L800S0V35) with ESMTP id com for ; Thu, 27 Dec 2001 13:19:11 -0500 content-class: urn:content-classes:message MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Subject: LOP operation Date: Thu, 27 Dec 2001 10:20:03 -0800 Message-ID: Thread-Topic: LOP operation Thread-Index: AcGPA2c/IxYCwj82RiOGMZlN1cHnOw== From: "Carl Cadwell" To: X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> My Understanding: In extensive discussions with Orin and the folks at TCM, LOP operation should only be used when operating the TSIO-550-E at or below 65% power. To do it at higher power settings is going to significantly shorten the life of the engine. If you are going to run at higher power settings, the fuel flow needs to be set to yield readings of 50-75 degrees ROP. The greatest danger zone is 50 degrees ROP to peak. It is my conclusion from reading and discussing this with the GAMI folks, that they claim there is no shortening of the life of the engine to run the engine at higher power settings lean of peak as long as you are using their injectors. TCM does not agree and TCM has to warranty the early cylinder failures. =20 Performing the power vs. temperature curve on the E model in my plane shows very little variance in the peak temperatures across the cylinders. So in my opinion, very little would be gained in using GAMI injectors. So currently I am running 75 degrees lean of peak at cruise. I am using 2400 rpm and 29" manifold pressure. I burn 15.5 gph. With 90 gallons of fuel I can fly 4 hours with 25 gallons of fuel remaining. My TAS speeds at various altitudes are:=20 9000 209 kts 18000 234 kts=09 21000 246 kts=09 25000 264 kts I used the following site for the calculations flying 3 cardinal directions and recording the GPS groundspeed. http://www.reacomp.com/true_airspeed/index.html=09 My TIT is typically 1510-1540. The hottest cylinder is #5 at 310. I adjust the oil door to keep the oil at 170. In climb, I use full rich, 30" and 2500 rpm and see 1200-1400 fpm. Hottest cylinder #5 is 370-380 And it runs very smoothly, even smoother now with my MT prop dynamically balanced. I also add 4 oz. of Marvel's Mystery Oil per 10 gallons. I make certain my oil temperature is 30 degrees or warmer before any start. My disclaimer: I am just a guy out in the sticks of Eastern Washington still trying to figure out life and having fun. Carl Cadwell =20 N25CL, IVP 120 hours >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://members.olsusa.com/mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please remember that purchases from the Builders' Bookstore assist with the management of the LML. Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>