X-Virus-Scanned: clean according to Sophos on Logan.com X-SpamCatcher-Score: 30 [X] Return-Path: Sender: To: lml@lancaironline.net Date: Wed, 21 Mar 2007 15:50:40 -0400 Message-ID: X-Original-Return-Path: Received: from vms048pub.verizon.net ([206.46.252.48] verified) by logan.com (CommuniGate Pro SMTP 5.1.7) with ESMTP id 1935024 for lml@lancaironline.net; Wed, 21 Mar 2007 13:38:55 -0400 Received: from [192.168.111.2] ([70.19.45.50]) by vms048.mailsrvcs.net (Sun Java System Messaging Server 6.2-6.01 (built Apr 3 2006)) with ESMTPA id <0JF900620KZCWZV4@vms048.mailsrvcs.net> for lml@lancaironline.net; Wed, 21 Mar 2007 12:38:02 -0500 (CDT) X-Original-Date: Wed, 21 Mar 2007 13:37:59 -0400 From: Kevin Kossi Subject: [LML] Re: carbureted lean-of-peak X-Original-To: Lancair Mailing List X-Original-Message-id: MIME-version: 1.0 (Apple Message framework v752.2) X-Mailer: Apple Mail (2.752.2) Content-type: multipart/alternative; boundary=Apple-Mail-44-770467262 --Apple-Mail-44-770467262 Content-Transfer-Encoding: quoted-printable Content-Type: text/plain; charset=WINDOWS-1252; delsp=yes; format=flowed This is what I have from Performance Engines: How to lean a High Performance Engine by: Performance Engines. Climb out full rich, full power to 6,000 feet (make sure all engine =20 parameters are within the correct temperature tolerances). Make sure you select a somewhat desolate area. (So you do not have to =20= worry about traffic that much). Preferably pick a day with little wind at your altitude. Engage your autopilot on a heading. Set up for 65% or less power. Suggest: 2400 rpm at 24=94 Make sure you keep a log of all this. A. Select Cylinder #1 EGT on your engine analyzer. B. Cut the mixture back one turn at a time and WAIT until the EGT =20 raises to a stabilized temperature (do not continue leaning until the temperature is =20 stabilized). The EGT will rise and subsequently stabilize with each turn of cut back on the mixture. C. Continue to cut back the mixture as stated in paragraph B until =20 you see the EGT stop climbing and start to drop. D. Immediately note the highest temperature attainable and =20 corresponding fuel flow at which Cylinder 1 stopped climbing and started descending. This cylinder has =20= reached its highest temperature attainable (PEAK EGT). E. Go to full rich. F. Select EGT cylinder #2. G. Wait for a stabilized temperature on your EGT cylinder #2. H. Repeat paragraphs A through E. on cylinders 2, 3, 4, 5, and 6. Now you have established the PEAK EGT for each cylinder. Each =20 aircraft will vary, especially experimentals. Now select the cylinder that peaked at the lowest temperature. This =20 is the CRITICAL cylinder. Let=92s suppose (and this is only a supposition) that the cylinder that =20= peaked at the lowest temperature was cylinder #5 at 1375o degrees F. This means: A. Your critical cylinder is #5, and.. B. For any cruise power setting (up to 75%) the EGT should be 100o F =20 cool of this critical cylinders peak EGT. Given the aforementioned all other cylinders will be richer =20= and therefore within a safe operating margin. C. For any higher power setting (i.e. take off), the EGT should be =20 150o to 200o degrees F. richer (cooler) of peak than established for the critical cylinder. If your =20 engine=92s set up can not achieve these temperatures you will have to change the fuel flow. By adhering to these policies you can extend the TBO of your engine. Performance Engines does not recommend running your engine lean of =20 peak (LOP) if the power setting is above 65% power. Furthermore, running LOP in excess of 65% =20= will void your warranty. (Lycoming engines may not be operated lean of peak per the =20 manufacturers=92 recommendations.). Please remember that to run lean of peak your aircraft must be =20 equipped with an engine analyzer that has downloading capability. Operation of a Performance Engine lean of peak without a downloadable =20= engine analyzer will void your warranty. Kevin Kossi Legacy 76% New York Continental IO-550-EXP 10:1 Single Lightspeed Single Slick Mag Hartzell HC-H3YF-2UFX/FC7391D-3X. Full feathering, counterweighted, 3 blade --Apple-Mail-44-770467262 Content-Transfer-Encoding: quoted-printable Content-Type: text/html; charset=WINDOWS-1252
This is what I = have from=A0Performance Engines:

How to lean a High Performance Engine by: Performance = Engines.
Climb out full = rich, full power to 6,000 feet (make sure all engine parameters are = within the
correct = temperature tolerances).
Make sure you = select a somewhat desolate area. (So you do not have to worry about = traffic
that = much).
Preferably pick = a day with little wind at your altitude.
Engage your autopilot on a = heading.
Set up for 65% = or less power. Suggest: 2400 rpm at 24=94
Make sure you keep a log of all = this.
A. Select = Cylinder #1 EGT on your engine analyzer.
B. Cut the mixture back one turn at a time and WAIT until the = EGT raises to a stabilized
temperature (do not continue leaning until the temperature is = stabilized). The EGT will rise and
subsequently stabilize with each turn of cut back on the = mixture.
C. Continue to = cut back the mixture as stated in paragraph B until you see the EGT = stop
climbing and = start to drop.
D. Immediately = note the highest temperature attainable and corresponding fuel flow at = which
Cylinder 1 = stopped climbing and started descending. This cylinder has reached its = highest
temperature = attainable (PEAK EGT).
E. Go to full = rich.
F. Select EGT = cylinder #2.
G. Wait for a = stabilized temperature on your EGT cylinder = #2.
H. Repeat = paragraphs A through E. on cylinders 2, 3, 4, 5, and = 6.
Now you have = established the PEAK EGT for each cylinder. Each aircraft will vary, = especially
experimentals.
Now select the = cylinder that peaked at the lowest temperature. This is the = CRITICAL cylinder.
Let=92s suppose = (and this is only a supposition) that the = cylinder that peaked at the lowest
temperature was cylinder #5 at 1375o = degrees F.
This = means:
A. Your = critical cylinder is #5, and..
B. For any cruise power setting (up to 75%) the EGT should be = 100o F cool of this critical = cylinders
peak EGT. Given = the aforementioned all other cylinders will be richer and therefore = within a safe
operating = margin.
C. For any = higher power setting (i.e. take off), the EGT should be = 150o to 200o = degrees F. richer
(cooler) of peak than established for the critical cylinder. = If your engine=92s set up can not
achieve these temperatures you will have to change the fuel = flow.
By adhering to = these policies you can extend the TBO of your = engine.
Performance = Engines does not recommend running your engine lean of peak (LOP) if the = power
setting is = above 65% power. Furthermore, running LOP in excess of 65% will void = your warranty.
(Lycoming = engines may not be operated lean of peak per the = manufacturers=92
recommendations.).
Please remember that to run lean of peak your aircraft must be = equipped with an engine
analyzer that = has downloading capability.
Operation of a Performance Engine lean of peak without a = downloadable engine analyzer will
void your warranty.

Kevin = Kossi
Legacy=A076%
New = York=A0
Continental IO-550-EXP
10:1=A0Single = Lightspeed=A0Single Slick Mag
Hartzell=A0 Full feathering, counterweighted, 3 = blade=A0

= --Apple-Mail-44-770467262--