X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Tue, 25 Apr 2006 09:18:59 -0400 Message-ID: X-Original-Return-Path: Received: from secure5.liveoakhosting.com ([64.49.254.21] verified) by logan.com (CommuniGate Pro SMTP 5.0.9) with ESMTPS id 1080186 for lml@lancaironline.net; Tue, 25 Apr 2006 08:26:00 -0400 Received-SPF: none receiver=logan.com; client-ip=64.49.254.21; envelope-from=walter@advancedpilot.com Received: (qmail 23269 invoked from network); 25 Apr 2006 07:24:55 -0500 Received: from 216-107-97-170.wan.networktel.net (HELO ?10.0.1.4?) (216.107.97.170) by rs5.liveoakhosting.com with SMTP; 25 Apr 2006 07:24:55 -0500 Mime-Version: 1.0 (Apple Message framework v623) In-Reply-To: References: Content-Type: multipart/alternative; boundary=Apple-Mail-1-156970430 X-Original-Message-Id: <7009f79c47bd819dcbe77aa00066aee8@advancedpilot.com> From: Walter Atkinson Subject: Re: [LML] P&W CHT X-Original-Date: Tue, 25 Apr 2006 07:24:54 -0500 X-Original-To: "Lancair Mailing List" X-Mailer: Apple Mail (2.623) --Apple-Mail-1-156970430 Content-Transfer-Encoding: quoted-printable Content-Type: text/plain; charset=ISO-8859-1; format=flowed One should keep in mind that those are very low compression engines=20 (6:1) which operate under relatively low ICPs. I work very hard to=20 keep my own personal P&W engines on my Twin Beech under 380. Prior to=20= doing that I replaced five cylinders in the first 200 hours of=20 operation. After adhering to the lower CHT, I have not replaced a=20 single cylinder in the last 800+ hours. I realize that anecdotal=20 evidence is a poor substitute for hard data, but it is in harmony with=20= the hard data. Those high CHTs are a result of poor cooling baffle=20 design. I have worked diligently to improve them with moderate=20 success. Walter On Apr 24, 2006, at 11:43 PM, Paul Lipps wrote: My airline pilot friend, who is building a Lionheart, told me what the=20= CHTs were=A0on the P&Ws he flew on the twin-engine Convair. Max CHT,=20 260C, 500F. METO, 232C, 450F. RECOMMENDED cruise, 204C, 400F. This was=20= the temperature that they were supposed to adjust their cowl flaps to=20 achieve during cruise! BTW, I was asked, on my first posting about CHT,=20= to reference=A0the source of my opinions, which I subsequently did. I=20 hope all that respond with other views=A0will do likewise.= --Apple-Mail-1-156970430 Content-Transfer-Encoding: quoted-printable Content-Type: text/enriched; charset=ISO-8859-1 One should keep in mind that those are very low compression engines (6:1) which operate under relatively low ICPs. I work very hard to keep my own personal P&W engines on my Twin Beech under 380. Prior to doing that I replaced five cylinders in the first 200 hours of operation. After adhering to the lower CHT, I have not replaced a single cylinder in the last 800+ hours. I realize that anecdotal evidence is a poor substitute for hard data, but it is in harmony with the hard data. Those high CHTs are a result of poor cooling baffle design. I have worked diligently to improve them with moderate success. Walter On Apr 24, 2006, at 11:43 PM, Paul Lipps wrote: ArialMy airline pilot friend, who is building a Lionheart, told me what the CHTs were=A0on the P&Ws he flew on the twin-engine Convair. Max CHT, 260C, 500F. METO, 232C, 450F. RECOMMENDED cruise, 204C, 400F. This was the temperature that they were supposed to adjust their cowl flaps to achieve during cruise! BTW, I was asked, on my first posting about CHT, to reference=A0the source of my opinions, which I subsequently did. I hope all that respond with other views=A0will do = likewise.= --Apple-Mail-1-156970430--