X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Wed, 20 Jun 2012 12:12:01 -0400 Message-ID: X-Original-Return-Path: Received: from nm28-vm0.access.bullet.mail.sp2.yahoo.com ([98.139.44.190] verified) by logan.com (CommuniGate Pro SMTP 5.4.5) with SMTP id 5609398 for lml@lancaironline.net; Wed, 20 Jun 2012 09:58:50 -0400 Received-SPF: none receiver=logan.com; client-ip=98.139.44.190; envelope-from=paulhershorin@bellsouth.net Received: from [98.139.44.100] by nm28.access.bullet.mail.sp2.yahoo.com with NNFMP; 20 Jun 2012 13:58:14 -0000 Received: from [98.139.44.91] by tm5.access.bullet.mail.sp2.yahoo.com with NNFMP; 20 Jun 2012 13:58:14 -0000 Received: from [127.0.0.1] by omp1028.access.mail.sp2.yahoo.com with NNFMP; 20 Jun 2012 13:58:14 -0000 X-Yahoo-Newman-Property: ymail-3 X-Yahoo-Newman-Id: 8500.22055.bm@omp1028.access.mail.sp2.yahoo.com Received: (qmail 86435 invoked by uid 60001); 20 Jun 2012 13:58:13 -0000 DomainKey-Signature:a=rsa-sha1; q=dns; c=nofws; s=s1024; d=bellsouth.net; h=X-YMail-OSG:Received:X-Mailer:Message-ID:Date:From:Subject:To:In-Reply-To:MIME-Version:Content-Type; b=MNXdJvNMFORG/g060gIi4sPwU6VEV42g9IgLyNBGjCUDrN9hPaMYXLAa40vdh7oNU04fHexY0tYBKKd7e03obkUxdAGZndngILVnjJwYO6dJmyiQ01lWtOimQGDfysAxaubpmxQqD/G81qTo3+GuMGsTlm3+eMTUGA6M56COJGc=; X-YMail-OSG: 93RTzqUVM1koCGJf7JR1Nm1BvndYRaImZ6XjpMsAyhqjawA 5J2P8vCferhlkmOcrgllfhGiGsODErEmpYULoLBKgfLCzYHuO.3eujMVYAbm KYxUtc521QuOktWULccUyzlvMlLQtStF6V_4Rej5jxdInfJiBxdDAaUsV6DX gTy6tb95iNo6CsLktgYAYNOy1XQ1_Wq7xJ80Iw9agyivWFQ_ray3ucW6fngU mOKHI6Q1k8AW.nvL4bA3D0eI4I03BQXO1Rr8Qc8wwoudD64cOl4kn_YAan7o zOFpXA6PHPxf88ThKhz7gRFf0YorFEVN2tKzyF4gQ1FHv1HCw6Z15gh2FXSB iEVDe24GA38DrnRLFp7Bi.MZskQwASUKiHoxDpOhEn0CKYnhQCglQFKiatsS gtaAI5mjzfssKPKmKnf__nY12fTepYJ8Q2kLL0c3jqA-- Received: from [98.77.127.140] by web83910.mail.sp1.yahoo.com via HTTP; Wed, 20 Jun 2012 06:58:13 PDT X-Mailer: YahooMailClassic/15.0.6 YahooMailWebService/0.8.118.349524 X-Original-Message-ID: <1340200693.71683.YahooMailClassic@web83910.mail.sp1.yahoo.com> X-Original-Date: Wed, 20 Jun 2012 06:58:13 -0700 (PDT) From: PAUL HERSHORIN Subject: Re: [LML] Re: Precision airmotive servo X-Original-To: Lancair Mailing List In-Reply-To: MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="257612794-1265295146-1340200693=:71683" --257612794-1265295146-1340200693=:71683 Content-Type: text/plain; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable I had to have the fuel flow on my servo increased three times before I felt= safe on take off performance figures. =A0 Paul Hershorin lnc2 360 --- On Wed, 6/20/12, Sky2high@aol.com wrote: From: Sky2high@aol.com Subject: [LML] Re: Precision airmotive servo To: lml@lancaironline.net Date: Wednesday, June 20, 2012, 9:46 AM Tom, =A0 My IO 320 (CR 9:1) uses 15.2 gph at takeoff (WOT, 2750 RPM, 700 MSL) and th= e leanest cyl=A0EGT is about 160 ROP.=A0 Base engine timing is 20 DBTDC (Du= al Plasma III EI). Hot day climb out at 135 KIAS will see CHTs at 380-390F.= =A0 I think=A0that the=A0flow is minimal but OK for me. =A0 The only proper way to adjust max flow=A0thru the servo is to do it on the = bench by a technician with special equipment. =A0 Scott Krueger =A0 In a message dated 6/20/2012 7:17:13 A.M. Central Daylight Time, n20087@yah= oo.com writes: Folks I believe my fuel servo is not delivering sufficient fuel to the engine in = the takeoff position. Why I say this is because the difference between the = peak EGT and the takeoff EGT is 70 degrees F on the leanest cylinder and 12= 0 on the richest.=A0 The book says this spread should be anywhere between 1= 50 and 200 degrees F.=A0 Why do I care you may ask.. Well my CHTs are too h= igh at full throttle takeoff.=A0 I have to work to keep them below 430.=A0 = I have done everything possible to maximize cooling airflow with little imp= rovement in the CHT situation.=A0=20 Anyhow, I would be interested in information from the group on the followin= g=20 Like to compare fuel flows at full throttle at close to sea level (mine is = between 15 and 16 gals/hr) Any info concerning experience with enriching the takeoff flow on the bendi= x style RSA-5AD1 servo (this setting is internal, I have found no reference= material on the procedure) Thanks Tom -- For archives and unsub http://mail.lancaironline.net:81/lists/lml/List.html --257612794-1265295146-1340200693=:71683 Content-Type: text/html; charset=iso-8859-1 Content-Transfer-Encoding: quoted-printable
I had to have the fuel flow on my servo = increased three times before I felt safe on take off performance figures.
 
Paul Hershorin
lnc2 360

--- On Wed, 6/20/12, Sky2high@aol.com <Sky2hi= gh@aol.com> wrote:

From: Sky2high@aol.com <Sky2high@aol.com>Subject: [LML] Re: Precision airmotive servo
To: lml@lancaironline.net=
Date: Wednesday, June 20, 2012, 9:46 AM

Tom,
 
My IO 320 (CR 9:1) uses 15.2 gph at takeoff (WOT, 2750 RPM, 700 MSL) a= nd the leanest cyl EGT is about 160 ROP.  Base engine timing is 2= 0 DBTDC (Dual Plasma III EI). Hot day climb out at 135 KIAS will see CHTs a= t 380-390F.  I think that the flow is minimal but OK for me.=
 
The only proper way to adjust max flow thru the servo is to do it= on the bench by a technician with special equipment.
 
Scott Krueger
 
In a message dated 6/20/2012 7:17:13 A.M. Central Daylight Time, n2008= 7@yahoo.com writes:
Folks

I believe my fuel servo is not delivering= sufficient fuel to the engine in the takeoff position. Why I say this is b= ecause the difference between the peak EGT and the takeoff EGT is 70 degree= s F on the leanest cylinder and 120 on the richest.  The book says thi= s spread should be anywhere between 150 and 200 degrees F.  Why do I c= are you may ask.. Well my CHTs are too high at full throttle takeoff. = I have to work to keep them below 430.  I have done everything possib= le to maximize cooling airflow with little improvement in the CHT situation= . 

Anyhow, I would be interested in information from the group= on the following

Like to compare fuel flows at full throttle at cl= ose to sea level (mine is between 15 and 16 gals/hr)
Any info concerning experience with enriching the takeoff flow on the bendix style RSA-5AD1 se= rvo (this setting is internal, I have found no reference material on the pr= ocedure)

Thanks

Tom
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