X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Fri, 17 Oct 2008 21:03:34 -0400 Message-ID: X-Original-Return-Path: Received: from web51012.mail.re2.yahoo.com ([206.190.39.155] verified) by logan.com (CommuniGate Pro SMTP 5.2.8) with SMTP id 3216865 for lml@lancaironline.net; Fri, 17 Oct 2008 08:23:52 -0400 Received: (qmail 20296 invoked by uid 60001); 17 Oct 2008 12:23:52 -0000 DomainKey-Signature: a=rsa-sha1; q=dns; c=nofws; s=s1024; d=swbell.net; h=X-YMail-OSG:Received:X-Mailer:Date:From:Reply-To:Subject:To:In-Reply-To:MIME-Version:Content-Type:Message-ID; b=T+nn86QjJqnn3HBKFa0KzakhQE0qSgkHEhc/MiYNqf1yPTifTkIE9HDoGpwbrs0wyHmce47B36AzL6PpkyRKeHlxlhSctfZU1htcq7+VvdiauPI6RAfH3Hr5NN6OSxPo9miSpbJ+cpvFX9fiuZarFISgmnc4NIk35vDvlI/2/q4=; X-YMail-OSG: PtFRuwcVM1nn4Ra1lOukYMqANcqQB9FOLHmn3jRA3Ewq3ckMfEo9J6AmDdzzbsBKHth0s7C1Lh2kd8YnJqukCtvS9WlLdTHwuhRMJW1Q5bC.uk9IB3nxWkLMJ4wy6z56jDvZWjIfrAp_P01.0gOHL8MtYW.FmM66rMwZ2Ciurg54uL1lvkHoKlbQrr0- Received: from [208.189.200.2] by web51012.mail.re2.yahoo.com via HTTP; Fri, 17 Oct 2008 05:23:51 PDT X-Mailer: YahooMailWebService/0.7.247.3 X-Original-Date: Fri, 17 Oct 2008 05:23:51 -0700 (PDT) From: Dr Andre Katz Reply-To: bu131@swbell.net Subject: Re: [LML] Re: IO-550N take off fuel flow X-Original-To: Lancair Mailing List In-Reply-To: MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="0-608046994-1224246231=:18580" X-Original-Message-ID: <949204.18580.qm@web51012.mail.re2.yahoo.com> --0-608046994-1224246231=:18580 Content-Type: text/plain; charset=windows-1252 Content-Transfer-Encoding: quoted-printable yes indeed when trying to increase the fuel flow in the ground by the non i= nstrumented technique we had a dead engine half way down the runway and by = luck we had a long runway to abort. be aware of this issue when fiddling wi= th the fuel flow control. ak --- On Fri, 10/17/08, Michael Newman wrote: From: Michael Newman Subject: [LML] Re: IO-550N take off fuel flow To: lml@lancaironline.net Date: Friday, October 17, 2008, 1:25 AM I think the book number is 41 GPH (check to be sure). In my IV-P I had fuel= flows similar to yours at takeoff and had cooling problems in climb. Incre= asing the fuel flow to the book number gave a richer mixture in climb and t= he CHTs started to stay below 400 in a 31 inch MP extended climb. =A0 We were not able to set this accurately at the shop (couldn=92t hold the pl= ane back safely). We had to set it and then and takeoff to fine tune it. We= discovered that increasing the Fuel Flow beyond the book numbers causes th= e engine to die when full power is applied at takeoff. =A0 I cannot speak to the high altitude airport issues. I would like to underst= and how that would be different than climb through those altitudes. =A0 From: John C. Bohn [mailto:JohnB@agcheattransfer.com]=20 Sent: Wednesday, October 15, 2008 1:39 AM To: lml@lancaironline.net Subject: RE: [LML] IO-550N take off fuel flow =A0 I=92m getting 36-38 GPH take off flow on my TSIO-550E.=A0 I was told this i= s too low but I don=92t believe it.=A0 If its higher than 38 it may cause a= problem during take off at some higher altitude airports or when changing = from LOP during landing=85.just my opinion. =A0 John C. Bohn N28487 4P Direct (Cell)- 503-887-2933 =A0 From: Lancair Mailing List [mailto:lml@lancaironline.net] On Behalf Of Fred= Moreno Sent: Sunday, October 12, 2008 7:49 PM To: lml@lancaironline.net Subject: [LML] IO-550N take off fuel flow =A0 I=A0 found an=A0article=A0for=A0Cirrus SR-22 owners suggesting that the tak= e off fuel flows on the IO-550N are set too low at the factory.=A0=20 =A0 As I recall the Continental fuel injection document calls for about 26 GPH = full rich full throttle, 2700 RPM.=A0=20 =A0 The Cirrus article recommended a minimum of 28 GPH to help lower peak cylin= der temperatures and pressures.=A0 Climb full rich, and then do the "big pu= ll" with the mixture knob all the way=A0into LOP territory.=A0 The table be= low shows how far to pull as a function of power setting. =A0 =A0 Lean of peak for the IO-550 N (8.5 compression ratio) horsepower is 15 time= s fuel flow in gallons per hour.=A0 This was the basis of the LOP flow rate= s in the table above.=A0 I figure that with 10:1 compression which produces= about 4-5% more horsepower, the number is about 15.6 horsepower per gallon= per hour. =A0 In my correspondence with a GAMI rep, the suggestion was a take off fuel fl= ow of 32 GPH when using 10:1 pistons.=A0=A0=20 =A0 What are you IO-550 operators getting for take off fuel flow??=A0 What reco= mmendations have you heard or seen? =A0 Fred Moreno Lancair IV, IO-550, awaiting a new Hartzell prop --0-608046994-1224246231=:18580 Content-Type: multipart/related; boundary="0-487682516-1224246231=:18580" --0-487682516-1224246231=:18580 Content-Type: text/html; charset=windows-1252 Content-Transfer-Encoding: quoted-printable
yes indeed when trying to increase the f= uel flow in the ground by the non instrumented technique we had a dead engi= ne half way down the runway and by luck we had a long runway to abort. be a= ware of this issue when fiddling with the fuel flow control.
ak

--- On Fri, 10/17/08, Michael Newman <mnewman@drago= nnorth.com> wrote:
From: Michael Newman <mnewman@dragonnorth.com><= BR>Subject: [LML] Re: IO-550N take off fuel flow
To: lml@lancaironline.n= et
Date: Friday, October 17, 2008, 1:25 AM

I think the book number is 41 GPH (check to= be sure). In my IV-P I had fuel flows similar to yours at takeoff and had = cooling problems in climb. Increasing the fuel flow to the book number gave= a richer mixture in climb and the CHTs started to stay below 400 in a 31 i= nch MP extended climb.

 

We were not able to set this accurately at = the shop (couldn=92t hold the plane back safely). We had to set it and then= and takeoff to fine tune it. We discovered that increasing the Fuel Flow b= eyond the book numbers causes the engine to die when full power is applied = at takeoff.

 

I cannot speak to the high altitude airport= issues. I would like to understand how that would be different than climb = through those altitudes.

 

From: John C. Bohn [mailto:JohnB@agcheattransfer.com= ]
Sent: Wednesday, October 15, 2008 1:39 AM
To: lml@la= ncaironline.net
Subject: RE: [LML] IO-550N take off fuel flow

 

I=92m getting 36-38 GPH take off flow on my TSIO= -550E.  I was told this is too low but I don=92t believe it.  If = its higher than 38 it may cause a problem during take off at some higher al= titude airports or when changing from LOP during landing=85.just my opinion= .

 

John C. Bohn<= /I>

N28487 4P=

Direct (Cell)- 503-8= 87-2933

 

From: Lancair Mailing = List [mailto:lml@lancaironline.net] On Behalf Of Fred Moreno
S= ent: Sunday, October 12, 2008 7:49 PM
To: lml@lancaironline.n= et
Subject: [LML] IO-550N take off fuel flow

 

I  found an article for Cirru= s SR-22 owners suggesting that the take off fuel flows on the IO-550N are s= et too low at the factory. 

 

As I recall the Continental fuel injection docume= nt calls for about 26 GPH full rich full throttle, 2700 RPM.  <= /DIV>

 

The Cirrus article recommended a minimum of 28 GP= H to help lower peak cylinder temperatures and pressures.  Climb full = rich, and then do the "big pull" with the mixture knob all the way int= o LOP territory.  The table below shows how far to pull as a function = of power setting.

 

3Dhttp://www.copapedia.org/images/e/ee/N5=

 

Lean of peak for the IO-550 N (8.5 = compression ratio) horsepower is 15 times fuel flow in gallons per hour.&nb= sp; This was the basis of the LOP flow rates in the table above.  I fi= gure that with 10:1 compression which produces about 4-5% more horsepower, = the number is about 15.6 horsepower per gallon per hour.

 

In my correspondence with a GAMI rep, the suggest= ion was a take off fuel flow of 32 GPH when using 10:1 pistons.  =

 

What are you IO-550 operators getting for take of= f fuel flow??  What recommendations have you heard or seen?

 

Fred Moreno

Lancair IV, IO-550, awaiting a new Hartzell prop<= /SPAN>

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