X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Tue, 03 Jun 2008 12:18:02 -0400 Message-ID: X-Original-Return-Path: Received: from [216.200.145.38] (HELO omta0103.mta.everyone.net) by logan.com (CommuniGate Pro SMTP 5.2.3) with ESMTP id 2951153 for lml@lancaironline.net; Tue, 03 Jun 2008 08:48:33 -0400 Received-SPF: none receiver=logan.com; client-ip=216.200.145.38; envelope-from=bknotts@buckeye-express.com Received: from dm37.mta.everyone.net (sj1-slb03-gw2 [172.16.1.96]) by omta0103.mta.everyone.net (Postfix) with ESMTP id 760573CCD8C for ; Tue, 3 Jun 2008 05:45:10 -0700 (PDT) X-Eon-Dm: dm37 Received: by dm37.mta.everyone.net (EON-AUTHRELAY2 - 48f0e224) id dm37.48447ea6.134e8 for ; Tue, 3 Jun 2008 05:47:53 -0700 X-Eon-Sig: AQK8DXBIRT15OlfMRgIAAAAB,f6c70695edbe0c1deed1c3c8b818c9ee X-Original-Message-ID: <48453D77.4040907@buckeye-express.com> X-Original-Date: Tue, 03 Jun 2008 08:47:51 -0400 From: "F. Barry Knotts" Reply-To: bknotts884@earthlink.net User-Agent: Thunderbird 2.0.0.14 (Windows/20080421) MIME-Version: 1.0 X-Original-To: Lancair Mail List Subject: [LML] Heat issues with a IV-P / TSIO-550E Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit Engine gurus...I recently purchased a Lancair IV-P (N4XE) that was completed only about 70 hours ago. The engine is a Performance Aero Engine rebuild of a stock Continental TSIO-550E. The only modifications were "Garrett larger turbos," Performance Aero Engine stock compression ratio pistons, GAMI injectors, chrome induction system, balancing and blueprinting. The prop is a Hartzell 3 blade SCIMITAR. The aircraft was flown by many (including myself) during the first 70 hours and the engine performed well. There has been a lot of tinkering with the engine setup during the first 70 hours. While doing HPAT training in the last 6-8 hours the temps have rapidly (and all together) climbed into the caution range necessitating full rich mixture and reductions in power to avoid going through the 1750d F EGT ceiling. The aircraft is at Lancair in Redmond and Tim Wilson and Tim Ong have been very diligent about working on the problem but have become stumped on how to proceed with shaking out the trouble. Continental and Ron Munson at Performance Aero Engines have not been really helpful. (Roughly: "Set it up by SID97-3D and it will run normally.") The timing, unmetered and metered pressures, and fuel flow have all been set up according to Continental Service Directive SID97-3D. All measurements have been through the Chelton engine monitor. When at full rich and the manifold pressure increased the temps rise in unison (all 14 of them, CHT's, EGT's and TIT's). Fuel flow transducer K value has been checked and re-entered. Baffling has been checked, but the rise in temperature is so rapid and consistent that Tim & Tim feel that it must be running lean somehow to show that temperature rise so quickly on advancement of the throttle. They have suggested that the fuel pump/metering unit be sent for rebuild/calibration. Although I'm not opposed to doing so, I thought I'd ask the experts here for any thoughts on things to check before taking that drastic step. My concern is; if the compression ratio is stock, the timing accurate, and the fuel flow at top of the recommended range (41.7 - 43.4 gal/hr), and the temps out of range, then one of the measurements must be incorrect. I'd like to check: RPM, manifold pressure, fuel flow and temps independently while the engine is running to determine if there is an indicator error through the Chilton EAU and display unit that is making setup inaccurate. Now the question: How, and in what order, would you suggest checking out these parameters? What else would you check? Thanks, in advance. Any suggestions on or off the list! Barry Knotts L-IVP, building...and new owner of a completed IV-P bknotts884@earthlink.net