X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml Date: Mon, 23 Nov 2009 12:08:03 -0500 Message-ID: X-Original-Return-Path: Received: from mail-yx0-f184.google.com ([209.85.210.184] verified) by logan.com (CommuniGate Pro SMTP 5.3c2) with ESMTP id 3985223 for lml@lancaironline.net; Sat, 21 Nov 2009 23:20:29 -0500 Received-SPF: pass receiver=logan.com; client-ip=209.85.210.184; envelope-from=dballin@gmail.com Received: by yxe14 with SMTP id 14so672760yxe.7 for ; Sat, 21 Nov 2009 20:19:55 -0800 (PST) DomainKey-Signature: a=rsa-sha1; c=nofws; d=gmail.com; s=gamma; h=mime-version:reply-to:date:message-id:subject:from:to:content-type; b=eA+e5cSzsN6vSJMLXCXzbsOy9vZKR3d8AIb0PODaMDqqciy4EyCvR2Wdzd3fSDmxPr +mDNNy8jpHZzTZ+IJ+Fn9TkeHhI/CXO1uhD/ul7yTcYpEJ4/VbZiyIb6IMf/UBr2L4Gn F2oJkk5/8QaQ7TQBZGk9q3KWQHzbVL9FXVxQM= MIME-Version: 1.0 Received: by 10.90.38.9 with SMTP id l9mr4871559agl.31.1258863595913; Sat, 21 Nov 2009 20:19:55 -0800 (PST) Reply-To: dballin@gmail.com X-Original-Date: Sat, 21 Nov 2009 20:19:55 -0800 X-Original-Message-ID: Subject: Fuel Pressure question From: Dan Ballin X-Original-To: Lancair Mailing List Content-Type: multipart/alternative; boundary=0016361e845e7481fb0478ee05c8 --0016361e845e7481fb0478ee05c8 Content-Type: text/plain; charset=ISO-8859-1 A few questions have come up regarding fuel pressure while flight testing Ralph Love's Legacy, N122PT. It has an IO-550 with MT prop. We've had indications of high fuel pressure when the throttle is retarded (38-40 psi) in the pattern which is accompanied by engine roughness. All gets better when the mixture is leaned. Testing has been done in Redmond - so patterns about 4-5000 ft. So is this "normal" and just explained by the overly rich state due to altitude and leaning is the solution or is something else going on? Where should the fuel pressure be measured from? The unmetered side of the fuel metering unit or the metered side? and why. And lastly, where have you mounted the fuel pressure transducer? EI suggests the firewall, but that leads to a long fuel line and ? does that make any difference in the readings, dampening etc. Can you mount it closer or are the vibrations going to cause failure of the fitting and fuel leaking over hot cylinders? Any thoughts or comments will be appreciated. Thanks Dan Ballin LEG2 #286 --0016361e845e7481fb0478ee05c8 Content-Type: text/html; charset=ISO-8859-1 Content-Transfer-Encoding: quoted-printable A few questions have come up regarding fuel pressure while flight testing R= alph Love's Legacy, N122PT.=A0 It has an IO-550 with MT prop.=A0 We'= ;ve had indications of high fuel pressure when the throttle is retarded (38= -40 psi) in the pattern which is accompanied by engine roughness.=A0 All ge= ts better when the mixture is leaned.=A0 Testing has been done in Redmond -= so patterns about 4-5000 ft.=A0 So is this "normal" and just exp= lained by the overly rich state due to altitude and leaning is the solution= or is something else going on?=A0 Where should the fuel pressure be measur= ed from?=A0 The unmetered side of the fuel metering unit or the metered sid= e?=A0 and why. =A0=A0 And lastly, where have you mounted the fuel pressure = transducer?=A0 EI suggests the firewall, but that leads to a long fuel line= and ? does that make any difference in the readings, dampening etc.=A0 Can= you mount it closer or are the vibrations going to cause failure of the fi= tting and fuel leaking over hot cylinders?

Any thoughts or comments will be appreciated.

Thanks

Dan = Ballin
LEG2 #286
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