Engines-Archive.digest.vol-ap

January 19, 2007 - March 21, 2007



            For what it cost to develop, the customer could have bought a 
      brand new 
            O-360 engine and then some. 
            Archie
      
      
      href="http://www.matronics.com/Navigator?Engines-List">http://www.matro
      nics.com/Navigator?Engines-List
      href="http://forums.matronics.com">http://forums.matronics.com
      
      
________________________________________________________________________________
From: "Tim Warlick" <timwarlick(at)bellsouth.net>
Subject: 161 hp @ 2700 rpm 0200
Date: Jan 19, 2007
Ok Archie, how did you increase the bhp from 100 to 161? If you turbocharged it you should call it a TS0200. Tim Mobile, AL ________________________________________________________________________________
From: "Archie" <archie97(at)earthlink.net>
Subject: Re: 161 hp @ 2700 rpm 0200
Date: Jan 19, 2007
That would be cheating. Both engines were normally aspirated. ----- Original Message ----- From: Tim Warlick To: engines-list(at)matronics.com Sent: Friday, January 19, 2007 7:10 PM Subject: Engines-List: 161 hp @ 2700 rpm 0200 Ok Archie, how did you increase the bhp from 100 to 161? If you turbocharged it you should call it a TS0200. Tim Mobile, AL ________________________________________________________________________________
From: "jrc" <jrccea(at)bellsouth.net>
Subject: Re: 161 hp @ 2700 rpm 0200
Date: Jan 19, 2007
He increased the compression, increased the intake velocity, reduced the exhaust backpressure, and jacked the rpm way up. JimC ----- Original Message ----- From: Tim Warlick To: engines-list(at)matronics.com Sent: Friday, January 19, 2007 6:10 PM Subject: Engines-List: 161 hp @ 2700 rpm 0200 Ok Archie, how did you increase the bhp from 100 to 161? If you turbocharged it you should call it a TS0200. Tim ________________________________________________________________________________
From: "jrc" <jrccea(at)bellsouth.net>
Subject: Re: Archie -- stroked O-200?
Date: Jan 19, 2007
Monty, if you wanted to increase the power output of an O-200 in the 2700-2800 rpm range (for durations of about 1 minute), with continuous cruise rpm to be in the 2100-2300 rpm range, what modifications would you consider feasible? JimC ________________________________________________________________________________
From: Gosh2Fly(at)aol.com
Date: Jan 20, 2007
Subject: Re: lycoming dual mag D engine alternative mag question
Skip' I presently fly an Acro Sport with a 0320H2AD. I have used both the crank sensor with the elecr. unit. and 3000 series dual mag. The 3000 series mag was rebuilt and has not given me any trouble. I also use the SilverHawk fuel injection system on the 0320H2AD ________________________________________________________________________________
From: "Bob & Toodie Marshall" <rtmarshall(at)osbtown.com>
Subject: Re: Engines-List Digest: 0 Msgs - 01/21/07
Date: Jan 22, 2007
Hi Archie and or others, there was some discussion on the list last week about the C-0200 and 0360 cylinders to make 240 cubes. In order to accomplish this on the 0200 would one have to bore the case. What other issues occur ? Isn't the C 0240 a completely new engine? Thanks for any and all input. Bob ----- Original Message ----- From: "Engines-List Digest Server" <engines-list(at)matronics.com> Sent: Sunday, January 21, 2007 11:56 PM Subject: Engines-List Digest: 0 Msgs - 01/21/07 > * > > ================================================= > Online Versions of Today's List Digest Archive > ================================================= > > Today's complete Engines-List Digest can also be found in either of the > two Web Links listed below. The .html file includes the Digest formatted > in HTML for viewing with a web browser and features Hyperlinked Indexes > and Message Navigation. The .txt file includes the plain ASCII version > of the Engines-List Digest and can be viewed with a generic text editor > such as Notepad or with a web browser. > > HTML Version: > > > http://www.matronics.com/digest/digestview.php?Style=82701&View=html&Chapter 07-01-21&Archive=Engines > > Text Version: > > > http://www.matronics.com/digest/digestview.php?Style=82701&View=txt&Chapter 07-01-21&Archive=Engines > > > =============================================== > EMail Version of Today's List Digest Archive > =============================================== > > > ---------------------------------------------------------- > Engines-List Digest Archive > --- > Total Messages Posted Sun 01/21/07: 0 > ---------------------------------------------------------- > > > Today's Message Index: > ---------------------- > > > -- > > ________________________________________________________________________________
From: "jrc" <jrccea(at)bellsouth.net>
Subject: Re: Engines-List Digest: 0 Msgs - 01/21/07
Date: Jan 22, 2007
The O-240 and IO-240 are essentially a new engine. Some parts and accessories do interchange. ----- Original Message ----- From: "Bob & Toodie Marshall" <rtmarshall(at)osbtown.com> Sent: Monday, January 22, 2007 9:39 AM Subject: Engines-List: Re: Engines-List Digest: 0 Msgs - 01/21/07 > > > Hi Archie and or others, there was some discussion on the list last week > about the C-0200 and 0360 cylinders to make 240 cubes. In order to > accomplish this on the 0200 would one have to bore the case. What other > issues occur ? Isn't the C 0240 a completely new engine? Thanks for any > and all input. Bob ________________________________________________________________________________
From: "Archie" <archie97(at)earthlink.net>
Subject: Re: Engines-List Digest: 0 Msgs - 01/21/07
Date: Jan 22, 2007
As I recall, the IO-240 was developed for Cessna aircraft, then was put aside when Cessna went with the Lycoming. The are/were available for sale, but have never worked on one, other than the purchase of an OH and parts manual. I have never fitted O-360 cylinders to an O-200 case, so cannot help in that regard. Stopped R & D on aircraft engines inasmuch as I lost interest, and accomplished the original intent. My suspicions were correct in almost all cases. Strictly racing now. Archie ================================================== ----- Original Message ----- From: "jrc" <jrccea(at)bellsouth.net> Sent: Monday, January 22, 2007 2:19 PM Subject: Re: Engines-List: Re: Engines-List Digest: 0 Msgs - 01/21/07 > > The O-240 and IO-240 are essentially a new engine. Some parts and > accessories do interchange. > > ----- Original Message ----- > From: "Bob & Toodie Marshall" <rtmarshall(at)osbtown.com> > To: > Sent: Monday, January 22, 2007 9:39 AM > Subject: Engines-List: Re: Engines-List Digest: 0 Msgs - 01/21/07 > > >> >> >> Hi Archie and or others, there was some discussion on the list last week >> about the C-0200 and 0360 cylinders to make 240 cubes. In order to >> accomplish this on the 0200 would one have to bore the case. What other >> issues occur ? Isn't the C 0240 a completely new engine? Thanks for any >> and all input. Bob > > > ________________________________________________________________________________
Subject: Re: Induction leak
From: "john beirne" <jmcb(at)oceanfree.net>
Date: Jan 22, 2007
An Induction leak will cause that cylinder to run leaner, have a look in the exhaust ports and see if one or more of them is less blackened than the rest what you are looking for is grey/whiteish coating or any sign of over heating This is not conclusive but should point you in the right direction. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=89619#89619 ________________________________________________________________________________
From: "Gene Smith" <esmith6(at)satx.rr.com>
Subject: Continental 0200 engine
Date: Feb 08, 2007
Any one out there know what a Teledyne Continental 0200 engine weighs with all accessories including the oil and exhaust?..............Thanks..................Gene Smith. ________________________________________________________________________________
Date: Feb 08, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Continental 0200 engine
I don't know with accessories. Its dry weight is listed at 166, compared to the lightest of O-300 is 270. On 2/8/07, Gene Smith wrote: > > Any one out there know what a Teledyne Continental 0200 engine weighs with > all accessories including the oil and > exhaust?..............Thanks..................Gene > Smith. > - The Engines-List Email Forum - > Navigator to browse > page, > Photoshare, and much much more: > http://www.matronics.com/Navigator?Engines-List > - NEW MATRONICS WEB FORUMS - > the Web Forums! > http://forums.matronics.com > ________________________________________________________________________________
From: "jrc" <jrccea(at)bellsouth.net>
Subject: Re: Continental 0200 engine
Date: Feb 08, 2007
Depends upon which mags you're running, which exhaust, which accessories (light weight or stock, generator or alternator, vacuum pump, etc.) ----- Original Message ----- From: Gene Smith To: engines-list Sent: Thursday, February 08, 2007 10:30 AM Subject: Engines-List: Continental 0200 engine Any one out there know what a Teledyne Continental 0200 engine weighs with all accessories including the oil and exhaust?..............Thanks..................Gene Smith. ________________________________________________________________________________
Date: Feb 11, 2007
From: Dan Rogers <drogers(at)maf.org>
Subject: Cam Lobe wear
Hi Gary, Some long time ago, you wrote the quote below. I am trying to find the cause of rough running in a Lyc O360A4M that has good compression, good mags, good timing. It has about 1400 smoh over about 12 years. There were times during those years in which it sat for over a year at a time. Also, for most of that time, the oil cooler hoses were connected wrong so the oil ran quite hot. How can I prove that there is or isn't excessive cam lobe wear without tearing it all down?? Thanks, Dan Gary Casey wrote: > Often the first sign of cam wear is a rough > engine and inspection will show that the cam lobe is gone. For some > time the engine tolerated that much iron and didn't fail. > Gary Casey > >> ________________________________________________________________________________
From: Gary Casey <glcasey(at)adelphia.net>
Subject: Re: Cam Lobe wear
Date: Feb 12, 2007
Dan, Yes, a compression test will not indicate that you have a problem with the cam. If it is really bad a cranking compression ("differential" compression test) might show the problem. Crank the engine with the mags and fuel off and note the difference between compression strokes - it is quite easy to tell if one cylinder is really low. You can pull the valve covers and measure the valve lift and that is one way to get a reasonable picture of cam lobe wear. You have to be careful about the hydraulic lifters as if one is collapsed you won't get an accurate measurement, but I don't know how to accommodate that, I'm afraid. From what I've heard, by the time the engine is running rough and is low on power the lobe will be essentially wiped off, making this method very effective - and it only takes a few minutes. I've used a simple steel scale, but a dial indicator would be more accurate. However, if you want to get a real look at the cam lobes the only way is to remove a cylinder - I'm told that on a 4-cylinder you can remove just one and get a peak at all the lobes, but I've never tried. Removing a cylinder isn't a huge deal, but it is a pain. It might take a day's labor to get it apart, inspected and put all back together. If the engine had no symptoms and looking in the valve covers showed no obvious problem, but showed metal in the filter then one has to look inside. With metal in the filter something is going to have to come apart anyway. Gary Casey > > Hi Gary, > > Some long time ago, you wrote the quote below. > > I am trying to find the cause of rough running in a Lyc O360A4M > that has > good compression, good mags, good timing. It has about 1400 smoh over > about 12 years. There were times during those years in which it > sat for > over a year at a time. Also, for most of that time, the oil cooler > hoses were connected wrong so the oil ran quite hot. > > How can I prove that there is or isn't excessive cam lobe wear without > tearing it all down?? > > Thanks, > > Dan ________________________________________________________________________________
Date: Feb 12, 2007
From: "J. Mcculley" <mcculleyja(at)starpower.net>
Subject: Re: Engines-List Digest: 1 Msgs - 02/11/07
Dan, One easy check you can make is to remove the rocker box covers and make a comparison check of each valve rocker arm amount of travel(in other words, the valve stem total travel)as the engine is turned by hand through at least two full engine revolutions in firing order. If one or more cam lobes are seriously worn more than others, the associated valve will not open as fully as it should, compared to those with less or no wear. Jim -------------------------------------------------------------------------- Engines-List Digest Server wrote: > I am trying to find the cause of rough running in a Lyc O360A4M that has > good compression, good mags, good timing. It has about 1400 smoh over > about 12 years. There were times during those years in which it sat for > over a year at a time. Also, for most of that time, the oil cooler > hoses were connected wrong so the oil ran quite hot. > > How can I prove that there is or isn't excessive cam lobe wear without > tearing it all down?? > > Thanks, > > Dan > > > Gary Casey wrote: > >> Often the first sign of cam wear is a rough >>engine and inspection will show that the cam lobe is gone. For some >>time the engine tolerated that much iron and didn't fail. >>Gary Casey ________________________________________________________________________________
From: "Gene Smith" <esmith6(at)satx.rr.com>
Subject: Re: Cam Lobe wear
Date: Feb 12, 2007
Yes, remove a cylinder and use a strong bright light and look up in there...I removed #2, and you can see the lobes...The other choice (and the best) is to buy one of the oil analysis kits (around $10) and send off a sample of your oil, and through a Spectroanalysis system (S.O.A.P.) they can tell you which component is wearing excessively by the type and amount of metal in your oil...As you know the different internal parts of your engine has a different type of metal...i.e: bearings, crankshaft journals, valve guides, cam lobes and etc. Interesting thing here as to the importance of this test, the USAF takes a S.O.A.P. sample after each flight of a Jet Fighter, (esp. if it is single engine) and the aircraft will not be released for the next mission until the analysis is complete and deemed safe......................Hope this helps...Good luck.............................CHEERS!!!! Gene Smith RV-4 ----- Original Message ----- From: "Gary Casey" <glcasey(at)adelphia.net> Sent: Monday, February 12, 2007 7:45 AM Subject: Engines-List: Re: Cam Lobe wear > > Dan, > Yes, a compression test will not indicate that you have a problem > with the cam. If it is really bad a cranking compression > ("differential" compression test) might show the problem. Crank the > engine with the mags and fuel off and note the difference between > compression strokes - it is quite easy to tell if one cylinder is > really low. You can pull the valve covers and measure the valve lift > and that is one way to get a reasonable picture of cam lobe wear. > You have to be careful about the hydraulic lifters as if one is > collapsed you won't get an accurate measurement, but I don't know how > to accommodate that, I'm afraid. From what I've heard, by the time > the engine is running rough and is low on power the lobe will be > essentially wiped off, making this method very effective - and it > only takes a few minutes. I've used a simple steel scale, but a dial > indicator would be more accurate. However, if you want to get a real > look at the cam lobes the only way is to remove a cylinder - I'm told > that on a 4-cylinder you can remove just one and get a peak at all > the lobes, but I've never tried. Removing a cylinder isn't a huge > deal, but it is a pain. It might take a day's labor to get it apart, > inspected and put all back together. If the engine had no symptoms > and looking in the valve covers showed no obvious problem, but showed > metal in the filter then one has to look inside. With metal in the > filter something is going to have to come apart anyway. > > Gary Casey > > > > Hi Gary, > > > > Some long time ago, you wrote the quote below. > > > > I am trying to find the cause of rough running in a Lyc O360A4M > > that has > > good compression, good mags, good timing. It has about 1400 smoh over > > about 12 years. There were times during those years in which it > > sat for > > over a year at a time. Also, for most of that time, the oil cooler > > hoses were connected wrong so the oil ran quite hot. > > > > How can I prove that there is or isn't excessive cam lobe wear without > > tearing it all down?? > > > > Thanks, > > > > Dan > > ________________________________________________________________________________
Date: Feb 12, 2007
From: Dan Rogers <drogers(at)maf.org>
Subject: Re: Cam Lobe wear
Thanks to Gary, Jim, Aaron,and Gene. Actually, I already have one cyl off for other reasons and didn't even think to try and look inside!!! The only real symptom right now casting a question on the cam is roughness that is not explained by anything else. We did and oil analysis about 8 hours ago and some metals were high but not real bad. There has not been any visible metal in the filter. Thanks again, everybody, Dan Dan Rogers wrote: > > Hi Gary, > > Some long time ago, you wrote the quote below. > > I am trying to find the cause of rough running in a Lyc O360A4M that has > good compression, good mags, good timing. It has about 1400 smoh over > about 12 years. There were times during those years in which it sat for > over a year at a time. Also, for most of that time, the oil cooler > hoses were connected wrong so the oil ran quite hot. > > How can I prove that there is or isn't excessive cam lobe wear without > tearing it all down?? > > Thanks, > > Dan > > > > Gary Casey wrote: >> Often the first sign of cam wear is a rough engine and inspection >> will show that the cam lobe is gone. For some time the engine >> tolerated that much iron and didn't fail. Gary Casey >> >>> > > > > > > ________________________________________________________________________________
Date: Feb 12, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Cam Lobe wear
Disagree on the oil analysis. Cam and lifters spall off relatively large chunks of metal, that are not microscopic and never burned in the spectrograph. You may see slightly elevated iron, but nothing startling, but you will see specks of iron in the oil filter. Went through this on my own IO-360 in 2001. KM, A&P/IA On 2/12/07, Gene Smith wrote: > > Yes, remove a cylinder and use a strong bright light and look up in > there...I removed #2, and you can see the lobes...The other choice (and the > best) is to buy one of the oil analysis kits (around $10) and send off a > sample of your oil, and through a Spectroanalysis system (S.O.A.P.) they can > tell you which component is wearing excessively by the type and amount of > metal in your oil...As you know the different internal parts of your engine > has a different type of metal...i.e: bearings, crankshaft journals, valve > guides, cam lobes and etc. > > Interesting thing here as to the importance of this test, the USAF takes a > S.O.A.P. sample after each flight of a Jet Fighter, (esp. if it is single > engine) and the aircraft will not be released for the next mission until the > analysis is complete and deemed safe......................Hope this > helps...Good luck.............................CHEERS!!!! > > Gene Smith > RV-4 > > > ----- Original Message ----- > From: "Gary Casey" <glcasey(at)adelphia.net> > To: > Sent: Monday, February 12, 2007 7:45 AM > Subject: Engines-List: Re: Cam Lobe wear > > > > > > Dan, > > Yes, a compression test will not indicate that you have a problem > > with the cam. If it is really bad a cranking compression > > ("differential" compression test) might show the problem. Crank the > > engine with the mags and fuel off and note the difference between > > compression strokes - it is quite easy to tell if one cylinder is > > really low. You can pull the valve covers and measure the valve lift > > and that is one way to get a reasonable picture of cam lobe wear. > > You have to be careful about the hydraulic lifters as if one is > > collapsed you won't get an accurate measurement, but I don't know how > > to accommodate that, I'm afraid. From what I've heard, by the time > > the engine is running rough and is low on power the lobe will be > > essentially wiped off, making this method very effective - and it > > only takes a few minutes. I've used a simple steel scale, but a dial > > indicator would be more accurate. However, if you want to get a real > > look at the cam lobes the only way is to remove a cylinder - I'm told > > that on a 4-cylinder you can remove just one and get a peak at all > > the lobes, but I've never tried. Removing a cylinder isn't a huge > > deal, but it is a pain. It might take a day's labor to get it apart, > > inspected and put all back together. If the engine had no symptoms > > and looking in the valve covers showed no obvious problem, but showed > > metal in the filter then one has to look inside. With metal in the > > filter something is going to have to come apart anyway. > > > > Gary Casey > > > > > > Hi Gary, > > > > > > Some long time ago, you wrote the quote below. > > > > > > I am trying to find the cause of rough running in a Lyc O360A4M > > > that has > > > good compression, good mags, good timing. It has about 1400 smoh over > > > about 12 years. There were times during those years in which it > > > sat for > > > over a year at a time. Also, for most of that time, the oil cooler > > > hoses were connected wrong so the oil ran quite hot. > > > > > > How can I prove that there is or isn't excessive cam lobe wear without > > > tearing it all down?? > > > > > > Thanks, > > > > > > Dan > > > > > > > > > > ________________________________________________________________________________
From: "Gene Smith" <esmith6(at)satx.rr.com>
Subject: Re: Cam Lobe wear
Date: Feb 12, 2007
Kelly, You seem like you have experience in this area and are knowledgeable about the subject....Educate me about this, if an engine sets up unpickled for a year, I understand from friends of mine that rust forms on the lobes, and when started again, rust flakes off and contaminates the oil system, then acts as pumice...Does this rust not show up on a spectrograph sample?..One Tripacer owner neglected to change oil very often (if at all) and complained of the engine not running right...I later saw the camshaft and there was only "nubbins" left...I don't see how the valves functioned at all...I've said this before, so will use this opportunity to mention it again, the cheapest thing you can buy for your engine is OIL, and change it often...I know the book says change at 50 hours, but I take a good look at mine at 25 hours and if it exhibits the slightest darkness, then out it goes...One step further, I use a 50/50 mix of Aeroshell and Mobil-I 15/w50, and after 1500 hours, have had no problems at all...I do not advocate any of you out there to use this mixture, especially certified aircraft...It is a personal thing with me..........Kelly, thanks for your inputs...............CHEERS!!!! Gene Smith RV-4 ----- Original Message ----- From: "Kelly McMullen" <apilot2(at)gmail.com> Sent: Monday, February 12, 2007 3:23 PM Subject: Re: Engines-List: Re: Cam Lobe wear > > Disagree on the oil analysis. Cam and lifters spall off relatively > large chunks of metal, that are not microscopic and never burned in > the spectrograph. You may see slightly elevated iron, but nothing > startling, but you will see specks of iron in the oil filter. Went > through this on my own IO-360 in 2001. > KM, > A&P/IA > > On 2/12/07, Gene Smith wrote: > > > > Yes, remove a cylinder and use a strong bright light and look up in > > there...I removed #2, and you can see the lobes...The other choice (and the > > best) is to buy one of the oil analysis kits (around $10) and send off a > > sample of your oil, and through a Spectroanalysis system (S.O.A.P.) they can > > tell you which component is wearing excessively by the type and amount of > > metal in your oil...As you know the different internal parts of your engine > > has a different type of metal...i.e: bearings, crankshaft journals, valve > > guides, cam lobes and etc. > > > > Interesting thing here as to the importance of this test, the USAF takes a > > S.O.A.P. sample after each flight of a Jet Fighter, (esp. if it is single > > engine) and the aircraft will not be released for the next mission until the > > analysis is complete and deemed safe......................Hope this > > helps...Good luck.............................CHEERS!!!! > > > > Gene Smith > > RV-4 > > > > > > > > ----- Original Message ----- > > From: "Gary Casey" <glcasey(at)adelphia.net> > > To: > > Sent: Monday, February 12, 2007 7:45 AM > > Subject: Engines-List: Re: Cam Lobe wear > > > > > > > > > > Dan, > > > Yes, a compression test will not indicate that you have a problem > > > with the cam. If it is really bad a cranking compression > > > ("differential" compression test) might show the problem. Crank the > > > engine with the mags and fuel off and note the difference between > > > compression strokes - it is quite easy to tell if one cylinder is > > > really low. You can pull the valve covers and measure the valve lift > > > and that is one way to get a reasonable picture of cam lobe wear. > > > You have to be careful about the hydraulic lifters as if one is > > > collapsed you won't get an accurate measurement, but I don't know how > > > to accommodate that, I'm afraid. From what I've heard, by the time > > > the engine is running rough and is low on power the lobe will be > > > essentially wiped off, making this method very effective - and it > > > only takes a few minutes. I've used a simple steel scale, but a dial > > > indicator would be more accurate. However, if you want to get a real > > > look at the cam lobes the only way is to remove a cylinder - I'm told > > > that on a 4-cylinder you can remove just one and get a peak at all > > > the lobes, but I've never tried. Removing a cylinder isn't a huge > > > deal, but it is a pain. It might take a day's labor to get it apart, > > > inspected and put all back together. If the engine had no symptoms > > > and looking in the valve covers showed no obvious problem, but showed > > > metal in the filter then one has to look inside. With metal in the > > > filter something is going to have to come apart anyway. > > > > > > Gary Casey > > > > > > > > Hi Gary, > > > > > > > > Some long time ago, you wrote the quote below. > > > > > > > > I am trying to find the cause of rough running in a Lyc O360A4M > > > > that has > > > > good compression, good mags, good timing. It has about 1400 smoh over > > > > about 12 years. There were times during those years in which it > > > > sat for > > > > over a year at a time. Also, for most of that time, the oil cooler > > > > hoses were connected wrong so the oil ran quite hot. > > > > > > > > How can I prove that there is or isn't excessive cam lobe wear without > > > > tearing it all down?? > > > > > > > > Thanks, > > > > > > > > Dan > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
Date: Feb 12, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Cam Lobe wear
What happens is a bit of rust or imperfection in the nitride layer causes a breakthrough to softer metal, on either cam or follower or both. Once that happens metal comes off quickly in relatively large particles..ones you can see. Oil analysis only detects metals at the microscopic size, that are vaporized in the spectrograph. Larger particles don't make it from the bottom of the sump, typically. My cam disintegrated, and luckily I was cutting the filter and saw the metal, and had to pull the oil pump for the AD on that and found it badly scored from the metal, so it was tear down time. I kept the cam and lifters as examples. I got to buy a replacement crank, new cam and lifters, and a new prop hub out of that episode...not all because of the cam, but from what I found on teardown. The good part is new prop hub I bought in 2002 is exempt from the current AD just issued this year. One gets very intimate with the details when you are building an engine for a type certified plane that you plan to fly, and may eventually sell to someone else, who will have your name in the logbooks as the mechanic that authorized its return to service, and may sue you 20 years later because it quit on them, even though they are 8 years and who knows how many hours past TBO. On 2/12/07, Gene Smith wrote: > > Kelly, > You seem like you have experience in this area and are knowledgeable about > the subject....Educate me about this, if an engine sets up unpickled for a > year, I understand from friends of mine that rust forms on the lobes, and > when started again, rust flakes off and contaminates the oil system, then > acts as pumice...Does this rust not show up on a spectrograph sample?..One > Tripacer owner neglected to change oil very often (if at all) and complained > of the engine not running right...I later saw the camshaft and there was > only "nubbins" left...I don't see how the valves functioned at all...I've > said this before, so will use this opportunity to mention it again, the > cheapest thing you can buy for your engine is OIL, and change it often...I > know the book says change at 50 hours, but I take a good look at mine at 25 > hours and if it exhibits the slightest darkness, then out it goes...One step > further, I use a 50/50 mix of Aeroshell and Mobil-I 15/w50, and after 1500 > hours, have had no problems at all...I do not advocate any of you out there > to use this mixture, especially certified aircraft...It is a personal thing > with me..........Kelly, thanks for your inputs...............CHEERS!!!! > > Gene Smith > RV-4 > > > ----- Original Message ----- > From: "Kelly McMullen" <apilot2(at)gmail.com> > To: > Sent: Monday, February 12, 2007 3:23 PM > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > Disagree on the oil analysis. Cam and lifters spall off relatively > > large chunks of metal, that are not microscopic and never burned in > > the spectrograph. You may see slightly elevated iron, but nothing > > startling, but you will see specks of iron in the oil filter. Went > > through this on my own IO-360 in 2001. > > KM, > > A&P/IA > > > > On 2/12/07, Gene Smith wrote: > > > > > > Yes, remove a cylinder and use a strong bright light and look up in > > > there...I removed #2, and you can see the lobes...The other choice (and > the > > > best) is to buy one of the oil analysis kits (around $10) and send off a > > > sample of your oil, and through a Spectroanalysis system (S.O.A.P.) they > can > > > tell you which component is wearing excessively by the type and amount > of > > > metal in your oil...As you know the different internal parts of your > engine > > > has a different type of metal...i.e: bearings, crankshaft journals, > valve > > > guides, cam lobes and etc. > > > > > > Interesting thing here as to the importance of this test, the USAF takes > a > > > S.O.A.P. sample after each flight of a Jet Fighter, (esp. if it is > single > > > engine) and the aircraft will not be released for the next mission until > the > > > analysis is complete and deemed safe......................Hope this > > > helps...Good luck.............................CHEERS!!!! > > > > > > Gene Smith > > > RV-4 > > > > > > > > > > > > ----- Original Message ----- > > > From: "Gary Casey" <glcasey(at)adelphia.net> > > > To: > > > Sent: Monday, February 12, 2007 7:45 AM > > > Subject: Engines-List: Re: Cam Lobe wear > > > > > > > > > > > > > > Dan, > > > > Yes, a compression test will not indicate that you have a problem > > > > with the cam. If it is really bad a cranking compression > > > > ("differential" compression test) might show the problem. Crank the > > > > engine with the mags and fuel off and note the difference between > > > > compression strokes - it is quite easy to tell if one cylinder is > > > > really low. You can pull the valve covers and measure the valve lift > > > > and that is one way to get a reasonable picture of cam lobe wear. > > > > You have to be careful about the hydraulic lifters as if one is > > > > collapsed you won't get an accurate measurement, but I don't know how > > > > to accommodate that, I'm afraid. From what I've heard, by the time > > > > the engine is running rough and is low on power the lobe will be > > > > essentially wiped off, making this method very effective - and it > > > > only takes a few minutes. I've used a simple steel scale, but a dial > > > > indicator would be more accurate. However, if you want to get a real > > > > look at the cam lobes the only way is to remove a cylinder - I'm told > > > > that on a 4-cylinder you can remove just one and get a peak at all > > > > the lobes, but I've never tried. Removing a cylinder isn't a huge > > > > deal, but it is a pain. It might take a day's labor to get it apart, > > > > inspected and put all back together. If the engine had no symptoms > > > > and looking in the valve covers showed no obvious problem, but showed > > > > metal in the filter then one has to look inside. With metal in the > > > > filter something is going to have to come apart anyway. > > > > > > > > Gary Casey > > > > > > > > > > Hi Gary, > > > > > > > > > > Some long time ago, you wrote the quote below. > > > > > > > > > > I am trying to find the cause of rough running in a Lyc O360A4M > > > > > that has > > > > > good compression, good mags, good timing. It has about 1400 smoh > over > > > > > about 12 years. There were times during those years in which it > > > > > sat for > > > > > over a year at a time. Also, for most of that time, the oil cooler > > > > > hoses were connected wrong so the oil ran quite hot. > > > > > > > > > > How can I prove that there is or isn't excessive cam lobe wear > without > > > > > tearing it all down?? > > > > > > > > > > Thanks, > > > > > > > > > > Dan > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: "William Becker" <wbecker(at)centurytel.net>
Subject: Re: Cam Lobe wear
Date: Feb 12, 2007
Why not just use Aeroshell 15/50, which is 50% synthetic ? Bill B ----- Original Message ----- From: "Gene Smith" <esmith6(at)satx.rr.com> Sent: Monday, February 12, 2007 6:54 PM Subject: Re: Engines-List: Re: Cam Lobe wear > > Kelly, > You seem like you have experience in this area and are knowledgeable about > the subject....Educate me about this, if an engine sets up unpickled for a > year, I understand from friends of mine that rust forms on the lobes, and > when started again, rust flakes off and contaminates the oil system, then > acts as pumice...Does this rust not show up on a spectrograph sample?..One > Tripacer owner neglected to change oil very often (if at all) and > complained > of the engine not running right...I later saw the camshaft and there was > only "nubbins" left...I don't see how the valves functioned at all...I've > said this before, so will use this opportunity to mention it again, the > cheapest thing you can buy for your engine is OIL, and change it often...I > know the book says change at 50 hours, but I take a good look at mine at > 25 > hours and if it exhibits the slightest darkness, then out it goes...One > step > further, I use a 50/50 mix of Aeroshell and Mobil-I 15/w50, and after 1500 > hours, have had no problems at all...I do not advocate any of you out > there > to use this mixture, especially certified aircraft...It is a personal > thing > with me..........Kelly, thanks for your inputs...............CHEERS!!!! > > Gene Smith > RV-4 > > > ----- Original Message ----- > From: "Kelly McMullen" <apilot2(at)gmail.com> > To: > Sent: Monday, February 12, 2007 3:23 PM > Subject: Re: Engines-List: Re: Cam Lobe wear > > >> >> Disagree on the oil analysis. Cam and lifters spall off relatively >> large chunks of metal, that are not microscopic and never burned in >> the spectrograph. You may see slightly elevated iron, but nothing >> startling, but you will see specks of iron in the oil filter. Went >> through this on my own IO-360 in 2001. >> KM, >> A&P/IA >> >> On 2/12/07, Gene Smith wrote: >> > >> > Yes, remove a cylinder and use a strong bright light and look up in >> > there...I removed #2, and you can see the lobes...The other choice (and > the >> > best) is to buy one of the oil analysis kits (around $10) and send off >> > a >> > sample of your oil, and through a Spectroanalysis system (S.O.A.P.) >> > they > can >> > tell you which component is wearing excessively by the type and amount > of >> > metal in your oil...As you know the different internal parts of your > engine >> > has a different type of metal...i.e: bearings, crankshaft journals, > valve >> > guides, cam lobes and etc. >> > >> > Interesting thing here as to the importance of this test, the USAF >> > takes > a >> > S.O.A.P. sample after each flight of a Jet Fighter, (esp. if it is > single >> > engine) and the aircraft will not be released for the next mission >> > until > the >> > analysis is complete and deemed safe......................Hope this >> > helps...Good luck.............................CHEERS!!!! >> > >> > Gene Smith >> > RV-4 >> > >> > >> > >> > ----- Original Message ----- >> > From: "Gary Casey" <glcasey(at)adelphia.net> >> > To: >> > Sent: Monday, February 12, 2007 7:45 AM >> > Subject: Engines-List: Re: Cam Lobe wear >> > >> > >> > > >> > > Dan, >> > > Yes, a compression test will not indicate that you have a problem >> > > with the cam. If it is really bad a cranking compression >> > > ("differential" compression test) might show the problem. Crank the >> > > engine with the mags and fuel off and note the difference between >> > > compression strokes - it is quite easy to tell if one cylinder is >> > > really low. You can pull the valve covers and measure the valve lift >> > > and that is one way to get a reasonable picture of cam lobe wear. >> > > You have to be careful about the hydraulic lifters as if one is >> > > collapsed you won't get an accurate measurement, but I don't know how >> > > to accommodate that, I'm afraid. From what I've heard, by the time >> > > the engine is running rough and is low on power the lobe will be >> > > essentially wiped off, making this method very effective - and it >> > > only takes a few minutes. I've used a simple steel scale, but a dial >> > > indicator would be more accurate. However, if you want to get a real >> > > look at the cam lobes the only way is to remove a cylinder - I'm told >> > > that on a 4-cylinder you can remove just one and get a peak at all >> > > the lobes, but I've never tried. Removing a cylinder isn't a huge >> > > deal, but it is a pain. It might take a day's labor to get it apart, >> > > inspected and put all back together. If the engine had no symptoms >> > > and looking in the valve covers showed no obvious problem, but showed >> > > metal in the filter then one has to look inside. With metal in the >> > > filter something is going to have to come apart anyway. >> > > >> > > Gary Casey >> > > > >> > > > Hi Gary, >> > > > >> > > > Some long time ago, you wrote the quote below. >> > > > >> > > > I am trying to find the cause of rough running in a Lyc O360A4M >> > > > that has >> > > > good compression, good mags, good timing. It has about 1400 smoh > over >> > > > about 12 years. There were times during those years in which it >> > > > sat for >> > > > over a year at a time. Also, for most of that time, the oil cooler >> > > > hoses were connected wrong so the oil ran quite hot. >> > > > >> > > > How can I prove that there is or isn't excessive cam lobe wear > without >> > > > tearing it all down?? >> > > > >> > > > Thanks, >> > > > >> > > > Dan >> > > >> > > >> > > >> > > >> > >> > >> > >> > >> > >> > >> >> >> > > > -- > ________________________________________________________________________________
From: "Gene Smith" <esmith6(at)satx.rr.com>
Subject: Re: Cam Lobe wear
Date: Feb 12, 2007
Bill B., I am not familiar with that oil, and did not know it was 50% synthetic, but thanks for the info, I certainly will investigate the Aeroshell...I get the Mobil I for $4.00 a quart...Is there a significant difference in price, not that it makes much difference when you are dealing with an aircraft engine, you always want the best...I am reluctant to say this, but with all the fraud and lying going on in almost all aspects of our lives now days, I know for sure I'm getting 50% synthetic when I measure and mix it myself...In no way am I accusing Shell or any other aspect of aviation of wrong doing...I run Mobil I in everything I have, including the lawn mower...I have one auto that the manufacturer requires it...Another reason I use the Aeroshell in the aircraft mixture is because I'm not sure Mobil I has enough detergent, otherwise, I would use 100% Mobil I which is 100% synthetic..That is one slick stuff.......Thanks for the info......................CHEERS!!!! ----- Original Message ----- From: "William Becker" <wbecker(at)centurytel.net> Sent: Monday, February 12, 2007 9:20 PM Subject: Re: Engines-List: Re: Cam Lobe wear > > Why not just use Aeroshell 15/50, which is 50% synthetic ? Bill B > ----- Original Message ----- > From: "Gene Smith" <esmith6(at)satx.rr.com> > To: > Sent: Monday, February 12, 2007 6:54 PM > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > Kelly, > > You seem like you have experience in this area and are knowledgeable about > > the subject....Educate me about this, if an engine sets up unpickled for a > > year, I understand from friends of mine that rust forms on the lobes, and > > when started again, rust flakes off and contaminates the oil system, then > > acts as pumice...Does this rust not show up on a spectrograph sample?..One > > Tripacer owner neglected to change oil very often (if at all) and > > complained > > of the engine not running right...I later saw the camshaft and there was > > only "nubbins" left...I don't see how the valves functioned at all...I've > > said this before, so will use this opportunity to mention it again, the > > cheapest thing you can buy for your engine is OIL, and change it often...I > > know the book says change at 50 hours, but I take a good look at mine at > > 25 > > hours and if it exhibits the slightest darkness, then out it goes...One > > step > > further, I use a 50/50 mix of Aeroshell and Mobil-I 15/w50, and after 1500 > > hours, have had no problems at all...I do not advocate any of you out > > there > > to use this mixture, especially certified aircraft...It is a personal > > thing > > with me..........Kelly, thanks for your inputs...............CHEERS!!!! > > > > Gene Smith > > RV-4 > > > > > > ----- Original Message ----- > > From: "Kelly McMullen" <apilot2(at)gmail.com> > > To: > > Sent: Monday, February 12, 2007 3:23 PM > > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > >> > >> Disagree on the oil analysis. Cam and lifters spall off relatively > >> large chunks of metal, that are not microscopic and never burned in > >> the spectrograph. You may see slightly elevated iron, but nothing > >> startling, but you will see specks of iron in the oil filter. Went > >> through this on my own IO-360 in 2001. > >> KM, > >> A&P/IA > >> > >> On 2/12/07, Gene Smith wrote: > >> > > >> > Yes, remove a cylinder and use a strong bright light and look up in > >> > there...I removed #2, and you can see the lobes...The other choice (and > > the > >> > best) is to buy one of the oil analysis kits (around $10) and send off > >> > a > >> > sample of your oil, and through a Spectroanalysis system (S.O.A.P.) > >> > they > > can > >> > tell you which component is wearing excessively by the type and amount > > of > >> > metal in your oil...As you know the different internal parts of your > > engine > >> > has a different type of metal...i.e: bearings, crankshaft journals, > > valve > >> > guides, cam lobes and etc. > >> > > >> > Interesting thing here as to the importance of this test, the USAF > >> > takes > > a > >> > S.O.A.P. sample after each flight of a Jet Fighter, (esp. if it is > > single > >> > engine) and the aircraft will not be released for the next mission > >> > until > > the > >> > analysis is complete and deemed safe......................Hope this > >> > helps...Good luck.............................CHEERS!!!! > >> > > >> > Gene Smith > >> > RV-4 > >> > > >> > > >> > > >> > ----- Original Message ----- > >> > From: "Gary Casey" <glcasey(at)adelphia.net> > >> > To: > >> > Sent: Monday, February 12, 2007 7:45 AM > >> > Subject: Engines-List: Re: Cam Lobe wear > >> > > >> > > >> > > > >> > > Dan, > >> > > Yes, a compression test will not indicate that you have a problem > >> > > with the cam. If it is really bad a cranking compression > >> > > ("differential" compression test) might show the problem. Crank the > >> > > engine with the mags and fuel off and note the difference between > >> > > compression strokes - it is quite easy to tell if one cylinder is > >> > > really low. You can pull the valve covers and measure the valve lift > >> > > and that is one way to get a reasonable picture of cam lobe wear. > >> > > You have to be careful about the hydraulic lifters as if one is > >> > > collapsed you won't get an accurate measurement, but I don't know how > >> > > to accommodate that, I'm afraid. From what I've heard, by the time > >> > > the engine is running rough and is low on power the lobe will be > >> > > essentially wiped off, making this method very effective - and it > >> > > only takes a few minutes. I've used a simple steel scale, but a dial > >> > > indicator would be more accurate. However, if you want to get a real > >> > > look at the cam lobes the only way is to remove a cylinder - I'm told > >> > > that on a 4-cylinder you can remove just one and get a peak at all > >> > > the lobes, but I've never tried. Removing a cylinder isn't a huge > >> > > deal, but it is a pain. It might take a day's labor to get it apart, > >> > > inspected and put all back together. If the engine had no symptoms > >> > > and looking in the valve covers showed no obvious problem, but showed > >> > > metal in the filter then one has to look inside. With metal in the > >> > > filter something is going to have to come apart anyway. > >> > > > >> > > Gary Casey > >> > > > > >> > > > Hi Gary, > >> > > > > >> > > > Some long time ago, you wrote the quote below. > >> > > > > >> > > > I am trying to find the cause of rough running in a Lyc O360A4M > >> > > > that has > >> > > > good compression, good mags, good timing. It has about 1400 smoh > > over > >> > > > about 12 years. There were times during those years in which it > >> > > > sat for > >> > > > over a year at a time. Also, for most of that time, the oil cooler > >> > > > hoses were connected wrong so the oil ran quite hot. > >> > > > > >> > > > How can I prove that there is or isn't excessive cam lobe wear > > without > >> > > > tearing it all down?? > >> > > > > >> > > > Thanks, > >> > > > > >> > > > Dan > >> > > > >> > > > >> > > > >> > > > >> > > >> > > >> > > >> > > >> > > >> > > >> > >> > >> > > > > > > > > > > > > > > > > > > -- > > > > ________________________________________________________________________________
Date: Feb 12, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Cam Lobe wear
Don't let that Mobil 1 get anywhere near the airport. There was a big class action and AD against Mobil 1 aircraft oil, lots of folks didn't get the full cost of repairing damage that oil caused to engines, props, governors. Exxon Elite or AeroShell 15-50 are both semi synthetic. Both around 50-55 a case on sale. Exxon does on-line sale for every major aviation event like SnF and OSH and AOPA Expo with rebate of some sort to reach that price. They pay shipping(drop shipped from closest distributor). On 2/12/07, Gene Smith wrote: > > Bill B., > I am not familiar with that oil, and did not know it was 50% synthetic, but > thanks for the info, I certainly will investigate the Aeroshell...I get the > Mobil I for $4.00 a quart...Is there a significant difference in price, not > that it makes much difference when you are dealing with an aircraft engine, > you always want the best...I am reluctant to say this, but with all the > fraud and lying going on in almost all aspects of our lives now days, I know > for sure I'm getting 50% synthetic when I measure and mix it myself...In no > way am I accusing Shell or any other aspect of aviation of wrong doing...I > run Mobil I in everything I have, including the lawn mower...I have one auto > that the manufacturer requires it...Another reason I use the Aeroshell in > the aircraft mixture is because I'm not sure Mobil I has enough detergent, > otherwise, I would use 100% Mobil I which is 100% synthetic..That is one > slick stuff.......Thanks for the info......................CHEERS!!!! > > > ----- Original Message ----- > From: "William Becker" <wbecker(at)centurytel.net> > To: > Sent: Monday, February 12, 2007 9:20 PM > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > > Why not just use Aeroshell 15/50, which is 50% synthetic ? Bill B > > ----- Original Message ----- > > From: "Gene Smith" <esmith6(at)satx.rr.com> > > To: > > Sent: Monday, February 12, 2007 6:54 PM > > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > > > > > Kelly, > > > You seem like you have experience in this area and are knowledgeable > about > > > the subject....Educate me about this, if an engine sets up unpickled for > a > > > year, I understand from friends of mine that rust forms on the lobes, > and > > > when started again, rust flakes off and contaminates the oil system, > then > > > acts as pumice...Does this rust not show up on a spectrograph > sample?..One > > > Tripacer owner neglected to change oil very often (if at all) and > > > complained > > > of the engine not running right...I later saw the camshaft and there was > > > only "nubbins" left...I don't see how the valves functioned at > all...I've > > > said this before, so will use this opportunity to mention it again, the > > > cheapest thing you can buy for your engine is OIL, and change it > often...I > > > know the book says change at 50 hours, but I take a good look at mine at > > > 25 > > > hours and if it exhibits the slightest darkness, then out it goes...One > > > step > > > further, I use a 50/50 mix of Aeroshell and Mobil-I 15/w50, and after > 1500 > > > hours, have had no problems at all...I do not advocate any of you out > > > there > > > to use this mixture, especially certified aircraft...It is a personal > > > thing > > > with me..........Kelly, thanks for your inputs...............CHEERS!!!! > > > > > > Gene Smith > > > RV-4 > > > > > > > > > ----- Original Message ----- > > > From: "Kelly McMullen" <apilot2(at)gmail.com> > > > To: > > > Sent: Monday, February 12, 2007 3:23 PM > > > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > > > > >> > > >> Disagree on the oil analysis. Cam and lifters spall off relatively > > >> large chunks of metal, that are not microscopic and never burned in > > >> the spectrograph. You may see slightly elevated iron, but nothing > > >> startling, but you will see specks of iron in the oil filter. Went > > >> through this on my own IO-360 in 2001. > > >> KM, > > >> A&P/IA > > >> > > >> On 2/12/07, Gene Smith wrote: > > > >> > > > >> > Yes, remove a cylinder and use a strong bright light and look up in > > >> > there...I removed #2, and you can see the lobes...The other choice > (and > > > the > > >> > best) is to buy one of the oil analysis kits (around $10) and send > off > > >> > a > > >> > sample of your oil, and through a Spectroanalysis system (S.O.A.P.) > > >> > they > > > can > > >> > tell you which component is wearing excessively by the type and > amount > > > of > > >> > metal in your oil...As you know the different internal parts of your > > > engine > > >> > has a different type of metal...i.e: bearings, crankshaft journals, > > > valve > > >> > guides, cam lobes and etc. > > >> > > > >> > Interesting thing here as to the importance of this test, the USAF > > >> > takes > > > a > > >> > S.O.A.P. sample after each flight of a Jet Fighter, (esp. if it is > > > single > > >> > engine) and the aircraft will not be released for the next mission > > >> > until > > > the > > >> > analysis is complete and deemed safe......................Hope this > > >> > helps...Good luck.............................CHEERS!!!! > > >> > > > >> > Gene Smith > > >> > RV-4 > > >> > > > >> > > > >> > > > >> > ----- Original Message ----- > > >> > From: "Gary Casey" <glcasey(at)adelphia.net> > > >> > To: > > >> > Sent: Monday, February 12, 2007 7:45 AM > > >> > Subject: Engines-List: Re: Cam Lobe wear > > >> > > > >> > > > > >> > > > > >> > > Dan, > > >> > > Yes, a compression test will not indicate that you have a problem > > >> > > with the cam. If it is really bad a cranking compression > > >> > > ("differential" compression test) might show the problem. Crank > the > > >> > > engine with the mags and fuel off and note the difference between > > >> > > compression strokes - it is quite easy to tell if one cylinder is > > >> > > really low. You can pull the valve covers and measure the valve > lift > > >> > > and that is one way to get a reasonable picture of cam lobe wear. > > >> > > You have to be careful about the hydraulic lifters as if one is > > >> > > collapsed you won't get an accurate measurement, but I don't know > how > > >> > > to accommodate that, I'm afraid. From what I've heard, by the time > > >> > > the engine is running rough and is low on power the lobe will be > > >> > > essentially wiped off, making this method very effective - and it > > >> > > only takes a few minutes. I've used a simple steel scale, but a > dial > > >> > > indicator would be more accurate. However, if you want to get a > real > > >> > > look at the cam lobes the only way is to remove a cylinder - I'm > told > > >> > > that on a 4-cylinder you can remove just one and get a peak at all > > >> > > the lobes, but I've never tried. Removing a cylinder isn't a huge > > >> > > deal, but it is a pain. It might take a day's labor to get it > apart, > > >> > > inspected and put all back together. If the engine had no symptoms > > >> > > and looking in the valve covers showed no obvious problem, but > showed > > >> > > metal in the filter then one has to look inside. With metal in the > > >> > > filter something is going to have to come apart anyway. > > >> > > > > >> > > Gary Casey > > >> > > > > > >> > > > Hi Gary, > > >> > > > > > >> > > > Some long time ago, you wrote the quote below. > > >> > > > > > >> > > > I am trying to find the cause of rough running in a Lyc O360A4M > > >> > > > that has > > >> > > > good compression, good mags, good timing. It has about 1400 smoh > > > over > > >> > > > about 12 years. There were times during those years in which it > > >> > > > sat for > > >> > > > over a year at a time. Also, for most of that time, the oil > cooler > > >> > > > hoses were connected wrong so the oil ran quite hot. > > >> > > > > > >> > > > How can I prove that there is or isn't excessive cam lobe wear > > > without > > >> > > > tearing it all down?? > > >> > > > > > >> > > > Thanks, > > >> > > > > > >> > > > Dan > > >> > > > > >> > > > > >> > > > > >> > > > > >> > > > >> > > > >> > > > >> > > > >> > > > >> > > > >> > > >> > > >> > > > > > > > > > > > > > > > > > > > > > > > > > > > -- > > > > > > > > > > > > > ________________________________________________________________________________
From: "Gene Smith" <esmith6(at)satx.rr.com>
Subject: Re: Cam Lobe wear
Date: Feb 13, 2007
Kelly.......... Guess there is no end to this...Those so called damaged engines were all replaced by Mobil...It was a sludge problem so the operators said...They were all very large engines and commercial operators in Ca...Mobil was going to fight it, but because of Barrister costs and dragging it through the courts they decided it was cheaper to settle it by replacing the engines, and settling down time...They then removed the aviation oil from the market because they said they weren't making any money off it, but were just doing it for the convenience of general aviation, so it was removed...(Now Exxon and Shell are making 50% synthetic, is their syn. any better than Mobil's?)..Mobil then came out with the 15W50, but for autos only...I used the Mobil 1 Aviation Oil for years in a C-150 and never had any sludge problem...The engine went over 2000 hours before each of two overhauls and the inside of the case and moving parts were golden, not even black, and obviously no sludge...I now have an RV-4 with a Lycoming 0320(160HP) with 1500 hours using the synthetic as mentioned in the earlier thread...I popped a cylinder to see what was going on, and inside it was just as golden as the Cessna...I know because you are an A&P/IA you are concerned about certified aircraft owners using it...I advocate none of that at all...Remember, I am EXPERIMENTAL, and operate under different rules. Questions for you...Does a certified aircraft and engine have to use an "approved" oil like Exxon and Shell, or can they use any oil of their choice?..I know break-in oil is straight mineral oil, correct?..Why is this necessary for break-in? Enjoyed discussing this with you, and wish you all the luck in the world...Thanks for all your info and time, you are very knowledgeable, and informative...........CHEERS!!!! Gene Smith RV-4 ----- Original Message ----- From: "Kelly McMullen" <apilot2(at)gmail.com> Sent: Monday, February 12, 2007 11:28 PM Subject: Re: Engines-List: Re: Cam Lobe wear > > Don't let that Mobil 1 get anywhere near the airport. There was a big > class action and AD against Mobil 1 aircraft oil, lots of folks didn't > get the full cost of repairing damage that oil caused to engines, > props, governors. Exxon Elite or AeroShell 15-50 are both semi > synthetic. Both around 50-55 a case on sale. Exxon does on-line sale > for every major aviation event like SnF and OSH and AOPA Expo with > rebate of some sort to reach that price. They pay shipping(drop > shipped from closest distributor). > > On 2/12/07, Gene Smith wrote: > > > > Bill B., > > I am not familiar with that oil, and did not know it was 50% synthetic, but > > thanks for the info, I certainly will investigate the Aeroshell...I get the > > Mobil I for $4.00 a quart...Is there a significant difference in price, not > > that it makes much difference when you are dealing with an aircraft engine, > > you always want the best...I am reluctant to say this, but with all the > > fraud and lying going on in almost all aspects of our lives now days, I know > > for sure I'm getting 50% synthetic when I measure and mix it myself...In no > > way am I accusing Shell or any other aspect of aviation of wrong doing...I > > run Mobil I in everything I have, including the lawn mower...I have one auto > > that the manufacturer requires it...Another reason I use the Aeroshell in > > the aircraft mixture is because I'm not sure Mobil I has enough detergent, > > otherwise, I would use 100% Mobil I which is 100% synthetic..That is one > > slick stuff.......Thanks for the info......................CHEERS!!!! > > > > > > > > ----- Original Message ----- > > From: "William Becker" <wbecker(at)centurytel.net> > > To: > > Sent: Monday, February 12, 2007 9:20 PM > > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > > > > > > > Why not just use Aeroshell 15/50, which is 50% synthetic ? Bill B > > > ----- Original Message ----- > > > From: "Gene Smith" <esmith6(at)satx.rr.com> > > > To: > > > Sent: Monday, February 12, 2007 6:54 PM > > > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > > > > > > > > > Kelly, > > > > You seem like you have experience in this area and are knowledgeable > > about > > > > the subject....Educate me about this, if an engine sets up unpickled for > > a > > > > year, I understand from friends of mine that rust forms on the lobes, > > and > > > > when started again, rust flakes off and contaminates the oil system, > > then > > > > acts as pumice...Does this rust not show up on a spectrograph > > sample?..One > > > > Tripacer owner neglected to change oil very often (if at all) and > > > > complained > > > > of the engine not running right...I later saw the camshaft and there was > > > > only "nubbins" left...I don't see how the valves functioned at > > all...I've > > > > said this before, so will use this opportunity to mention it again, the > > > > cheapest thing you can buy for your engine is OIL, and change it > > often...I > > > > know the book says change at 50 hours, but I take a good look at mine at > > > > 25 > > > > hours and if it exhibits the slightest darkness, then out it goes...One > > > > step > > > > further, I use a 50/50 mix of Aeroshell and Mobil-I 15/w50, and after > > 1500 > > > > hours, have had no problems at all...I do not advocate any of you out > > > > there > > > > to use this mixture, especially certified aircraft...It is a personal > > > > thing > > > > with me..........Kelly, thanks for your inputs...............CHEERS!!!! > > > > > > > > Gene Smith > > > > RV-4 > > > > > > > > > > > > ----- Original Message ----- > > > > From: "Kelly McMullen" <apilot2(at)gmail.com> > > > > To: > > > > Sent: Monday, February 12, 2007 3:23 PM > > > > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > > > > > > > > >> > > > >> Disagree on the oil analysis. Cam and lifters spall off relatively > > > >> large chunks of metal, that are not microscopic and never burned in > > > >> the spectrograph. You may see slightly elevated iron, but nothing > > > >> startling, but you will see specks of iron in the oil filter. Went > > > >> through this on my own IO-360 in 2001. > > > >> KM, > > > >> A&P/IA > > > >> > > > >> On 2/12/07, Gene Smith wrote: > > > > > >> > > > > >> > Yes, remove a cylinder and use a strong bright light and look up in > > > >> > there...I removed #2, and you can see the lobes...The other choice > > (and > > > > the > > > >> > best) is to buy one of the oil analysis kits (around $10) and send > > off > > > >> > a > > > >> > sample of your oil, and through a Spectroanalysis system (S.O.A.P.) > > > >> > they > > > > can > > > >> > tell you which component is wearing excessively by the type and > > amount > > > > of > > > >> > metal in your oil...As you know the different internal parts of your > > > > engine > > > >> > has a different type of metal...i.e: bearings, crankshaft journals, > > > > valve > > > >> > guides, cam lobes and etc. > > > >> > > > > >> > Interesting thing here as to the importance of this test, the USAF > > > >> > takes > > > > a > > > >> > S.O.A.P. sample after each flight of a Jet Fighter, (esp. if it is > > > > single > > > >> > engine) and the aircraft will not be released for the next mission > > > >> > until > > > > the > > > >> > analysis is complete and deemed safe......................Hope this > > > >> > helps...Good luck.............................CHEERS!!!! > > > >> > > > > >> > Gene Smith > > > >> > RV-4 > > > >> > > > > >> > > > > >> > > > > >> > ----- Original Message ----- > > > >> > From: "Gary Casey" <glcasey(at)adelphia.net> > > > >> > To: > > > >> > Sent: Monday, February 12, 2007 7:45 AM > > > >> > Subject: Engines-List: Re: Cam Lobe wear > > > >> > > > > >> > > > > > > >> > > > > > >> > > Dan, > > > >> > > Yes, a compression test will not indicate that you have a problem > > > >> > > with the cam. If it is really bad a cranking compression > > > >> > > ("differential" compression test) might show the problem. Crank > > the > > > >> > > engine with the mags and fuel off and note the difference between > > > >> > > compression strokes - it is quite easy to tell if one cylinder is > > > >> > > really low. You can pull the valve covers and measure the valve > > lift > > > >> > > and that is one way to get a reasonable picture of cam lobe wear. > > > >> > > You have to be careful about the hydraulic lifters as if one is > > > >> > > collapsed you won't get an accurate measurement, but I don't know > > how > > > >> > > to accommodate that, I'm afraid. From what I've heard, by the time > > > >> > > the engine is running rough and is low on power the lobe will be > > > >> > > essentially wiped off, making this method very effective - and it > > > >> > > only takes a few minutes. I've used a simple steel scale, but a > > dial > > > >> > > indicator would be more accurate. However, if you want to get a > > real > > > >> > > look at the cam lobes the only way is to remove a cylinder - I'm > > told > > > >> > > that on a 4-cylinder you can remove just one and get a peak at all > > > >> > > the lobes, but I've never tried. Removing a cylinder isn't a huge > > > >> > > deal, but it is a pain. It might take a day's labor to get it > > apart, > > > >> > > inspected and put all back together. If the engine had no symptoms > > > >> > > and looking in the valve covers showed no obvious problem, but > > showed > > > >> > > metal in the filter then one has to look inside. With metal in the > > > >> > > filter something is going to have to come apart anyway. > > > >> > > > > > >> > > Gary Casey > > > >> > > > > > > >> > > > Hi Gary, > > > >> > > > > > > >> > > > Some long time ago, you wrote the quote below. > > > >> > > > > > > >> > > > I am trying to find the cause of rough running in a Lyc O360A4M > > > >> > > > that has > > > >> > > > good compression, good mags, good timing. It has about 1400 smoh > > > > over > > > >> > > > about 12 years. There were times during those years in which it > > > >> > > > sat for > > > >> > > > over a year at a time. Also, for most of that time, the oil > > cooler > > > >> > > > hoses were connected wrong so the oil ran quite hot. > > > >> > > > > > > >> > > > How can I prove that there is or isn't excessive cam lobe wear > > > > without > > > >> > > > tearing it all down?? > > > >> > > > > > > >> > > > Thanks, > > > >> > > > > > > >> > > > Dan > > > >> > > > > > >> > > > > > >> > > > > > >> > > > > > >> > > > > >> > > > > >> > > > > >> > > > > >> > > > > >> > > > > >> > > > >> > > > >> > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > -- > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
Date: Feb 13, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Cam Lobe wear
First, the Mobil 1 problem was not isolated to large engines. There were a lot of private, non-commercial operators. A friend had a Continental TSIO360 damaged. Mobil fought every claim through so-called court "masters". A lot of owners suffered uncompensated losses. The problem is that synthetic oil does not hold sludge in suspension the way mineral oil does. That sludge centrifuges out in the worst places like prop hubs, bottom and top end of the engine, sticking valves, etc. That is why the approved oils are at least 50% mineral oil. Whether break-in oil is needed or not is a separate subject. While you can use what you want in an experimental engine, keep in mind that a lot of experimentals are flying behind certified engines, and a lot of evidence supports sticking with approved oils. The technology for air-cooled aircraft engines hasn't changed in 50 years, even if you have a few ignition or fuel system improvements. Unless you are burning true unleaded auto fuel, pure synthetic oil is an unnecessary risk, in my opinion. The only "aircraft" engine approved for use of Mobil 1 was the Porsche PFM engine, and it had a lot of automotive features, since that was its origin. All the other aircraft use of that oil was by STC approval, which has been revoked. Certified aircraft must use manufacturer approved oil or STC approved oil. On 2/13/07, Gene Smith wrote: > > Kelly.......... Guess there is no end to this...Those so called damaged > engines were all replaced by Mobil...It was a sludge problem so the > operators said...They were all very large engines and commercial operators > in Ca...Mobil was going to fight it, but because of Barrister costs and > dragging it through the courts they decided it was cheaper to settle it by > replacing the engines, and settling down time...They then removed the > aviation oil from the market because they said they weren't making any money > off it, but were just doing it for the convenience of general aviation, so > it was removed...(Now Exxon and Shell are making 50% synthetic, is their > syn. any better than Mobil's?)..Mobil then came out with the 15W50, but for > autos only...I used the Mobil 1 Aviation Oil for years in a C-150 and never > had any sludge problem...The engine went over 2000 hours before each of two > overhauls and the inside of the case and moving parts were golden, not even > black, and obviously no sludge...I now have an RV-4 with a Lycoming > 0320(160HP) with 1500 hours using the synthetic as mentioned in the earlier > thread...I popped a cylinder to see what was going on, and inside it was > just as golden as the Cessna...I know because you are an A&P/IA you are > concerned about certified aircraft owners using it...I advocate none of that > at all...Remember, I am EXPERIMENTAL, and operate under different rules. > > Questions for you...Does a certified aircraft and engine have to use an > "approved" oil like Exxon and Shell, or can they use any oil of their > choice?..I know break-in oil is straight mineral oil, correct?..Why is this > necessary for break-in? > > Enjoyed discussing this with you, and wish you all the luck in the > world...Thanks for all your info and time, you are very knowledgeable, and > informative...........CHEERS!!!! > > Gene Smith > RV-4 > > > ----- Original Message ----- > From: "Kelly McMullen" <apilot2(at)gmail.com> > To: > Sent: Monday, February 12, 2007 11:28 PM > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > Don't let that Mobil 1 get anywhere near the airport. There was a big > > class action and AD against Mobil 1 aircraft oil, lots of folks didn't > > get the full cost of repairing damage that oil caused to engines, > > props, governors. Exxon Elite or AeroShell 15-50 are both semi > > synthetic. Both around 50-55 a case on sale. Exxon does on-line sale > > for every major aviation event like SnF and OSH and AOPA Expo with > > rebate of some sort to reach that price. They pay shipping(drop > > shipped from closest distributor). > > > > On 2/12/07, Gene Smith wrote: > > > > > > Bill B., > > > I am not familiar with that oil, and did not know it was 50% synthetic, > but > > > thanks for the info, I certainly will investigate the Aeroshell...I get > the > > > Mobil I for $4.00 a quart...Is there a significant difference in price, > not > > > that it makes much difference when you are dealing with an aircraft > engine, > > > you always want the best...I am reluctant to say this, but with all the > > > fraud and lying going on in almost all aspects of our lives now days, I > know > > > for sure I'm getting 50% synthetic when I measure and mix it myself...In > no > > > way am I accusing Shell or any other aspect of aviation of wrong > doing...I > > > run Mobil I in everything I have, including the lawn mower...I have one > auto > > > that the manufacturer requires it...Another reason I use the Aeroshell > in > > > the aircraft mixture is because I'm not sure Mobil I has enough > detergent, > > > otherwise, I would use 100% Mobil I which is 100% synthetic..That is one > > > slick stuff.......Thanks for the info......................CHEERS!!!! > > > > > > > > > > > > ----- Original Message ----- > > > From: "William Becker" <wbecker(at)centurytel.net> > > > To: > > > Sent: Monday, February 12, 2007 9:20 PM > > > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > > > > > > > > > > > > Why not just use Aeroshell 15/50, which is 50% synthetic ? Bill B > > > > ----- Original Message ----- > > > > From: "Gene Smith" <esmith6(at)satx.rr.com> > > > > To: > > > > Sent: Monday, February 12, 2007 6:54 PM > > > > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > > > > > > > > > > > > > > Kelly, > > > > > You seem like you have experience in this area and are knowledgeable > > > about > > > > > the subject....Educate me about this, if an engine sets up unpickled > for > > > a > > > > > year, I understand from friends of mine that rust forms on the > lobes, > > > and > > > > > when started again, rust flakes off and contaminates the oil system, > > > then > > > > > acts as pumice...Does this rust not show up on a spectrograph > > > sample?..One > > > > > Tripacer owner neglected to change oil very often (if at all) and > > > > > complained > > > > > of the engine not running right...I later saw the camshaft and there > was > > > > > only "nubbins" left...I don't see how the valves functioned at > > > all...I've > > > > > said this before, so will use this opportunity to mention it again, > the > > > > > cheapest thing you can buy for your engine is OIL, and change it > > > often...I > > > > > know the book says change at 50 hours, but I take a good look at > mine at > > > > > 25 > > > > > hours and if it exhibits the slightest darkness, then out it > goes...One > > > > > step > > > > > further, I use a 50/50 mix of Aeroshell and Mobil-I 15/w50, and > after > > > 1500 > > > > > hours, have had no problems at all...I do not advocate any of you > out > > > > > there > > > > > to use this mixture, especially certified aircraft...It is a > personal > > > > > thing > > > > > with me..........Kelly, thanks for your > inputs...............CHEERS!!!! > > > > > > > > > > Gene Smith > > > > > RV-4 > > > > > > > > > > > > > > > ----- Original Message ----- > > > > > From: "Kelly McMullen" <apilot2(at)gmail.com> > > > > > To: > > > > > Sent: Monday, February 12, 2007 3:23 PM > > > > > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > > > > > > > > > > > > >> > > > > >> Disagree on the oil analysis. Cam and lifters spall off relatively > > > > >> large chunks of metal, that are not microscopic and never burned in > > > > >> the spectrograph. You may see slightly elevated iron, but nothing > > > > >> startling, but you will see specks of iron in the oil filter. Went > > > > >> through this on my own IO-360 in 2001. > > > > >> KM, > > > > >> A&P/IA > > > > >> > > > > >> On 2/12/07, Gene Smith wrote: > > > > > > > >> > > > > > >> > Yes, remove a cylinder and use a strong bright light and look up > in > > > > >> > there...I removed #2, and you can see the lobes...The other > choice > > > (and > > > > > the > > > > >> > best) is to buy one of the oil analysis kits (around $10) and > send > > > off > > > > >> > a > > > > >> > sample of your oil, and through a Spectroanalysis system > (S.O.A.P.) > > > > >> > they > > > > > can > > > > >> > tell you which component is wearing excessively by the type and > > > amount > > > > > of > > > > >> > metal in your oil...As you know the different internal parts of > your > > > > > engine > > > > >> > has a different type of metal...i.e: bearings, crankshaft > journals, > > > > > valve > > > > >> > guides, cam lobes and etc. > > > > >> > > > > > >> > Interesting thing here as to the importance of this test, the > USAF > > > > >> > takes > > > > > a > > > > >> > S.O.A.P. sample after each flight of a Jet Fighter, (esp. if it > is > > > > > single > > > > >> > engine) and the aircraft will not be released for the next > mission > > > > >> > until > > > > > the > > > > >> > analysis is complete and deemed safe......................Hope > this > > > > >> > helps...Good luck.............................CHEERS!!!! > > > > >> > > > > > >> > Gene Smith > > > > >> > RV-4 > > > > >> > > > > > >> > > > > > >> > > > > > >> > ----- Original Message ----- > > > > >> > From: "Gary Casey" <glcasey(at)adelphia.net> > > > > >> > To: > > > > >> > Sent: Monday, February 12, 2007 7:45 AM > > > > >> > Subject: Engines-List: Re: Cam Lobe wear > > > > >> > > > > > >> > > > > > > > > >> > > > > > > >> > > Dan, > > > > >> > > Yes, a compression test will not indicate that you have a > problem > > > > >> > > with the cam. If it is really bad a cranking compression > > > > >> > > ("differential" compression test) might show the problem. > Crank > > > the > > > > >> > > engine with the mags and fuel off and note the difference > between > > > > >> > > compression strokes - it is quite easy to tell if one cylinder > is > > > > >> > > really low. You can pull the valve covers and measure the > valve > > > lift > > > > >> > > and that is one way to get a reasonable picture of cam lobe > wear. > > > > >> > > You have to be careful about the hydraulic lifters as if one is > > > > >> > > collapsed you won't get an accurate measurement, but I don't > know > > > how > > > > >> > > to accommodate that, I'm afraid. From what I've heard, by the > time > > > > >> > > the engine is running rough and is low on power the lobe will > be > > > > >> > > essentially wiped off, making this method very effective - and > it > > > > >> > > only takes a few minutes. I've used a simple steel scale, but > a > > > dial > > > > >> > > indicator would be more accurate. However, if you want to get > a > > > real > > > > >> > > look at the cam lobes the only way is to remove a cylinder - > I'm > > > told > > > > >> > > that on a 4-cylinder you can remove just one and get a peak at > all > > > > >> > > the lobes, but I've never tried. Removing a cylinder isn't a > huge > > > > >> > > deal, but it is a pain. It might take a day's labor to get it > > > apart, > > > > >> > > inspected and put all back together. If the engine had no > symptoms > > > > >> > > and looking in the valve covers showed no obvious problem, but > > > showed > > > > >> > > metal in the filter then one has to look inside. With metal in > the > > > > >> > > filter something is going to have to come apart anyway. > > > > >> > > > > > > >> > > Gary Casey > > > > >> > > > > > > > >> > > > Hi Gary, > > > > >> > > > > > > > >> > > > Some long time ago, you wrote the quote below. > > > > >> > > > > > > > >> > > > I am trying to find the cause of rough running in a Lyc > O360A4M > > > > >> > > > that has > > > > >> > > > good compression, good mags, good timing. It has about 1400 > smoh > > > > > over > > > > >> > > > about 12 years. There were times during those years in which > it > > > > >> > > > sat for > > > > >> > > > over a year at a time. Also, for most of that time, the oil > > > cooler > > > > >> > > > hoses were connected wrong so the oil ran quite hot. > > > > >> > > > > > > > >> > > > How can I prove that there is or isn't excessive cam lobe > wear > > > > > without > > > > >> > > > tearing it all down?? > > > > >> > > > > > > > >> > > > Thanks, > > > > >> > > > > > > > >> > > > Dan > > > > >> > > > > > > >> > > > > > > >> > > > > > > >> > > > > > > >> > > > > > >> > > > > > >> > > > > > >> > > > > > >> > > > > > >> > > > > > >> > > > > >> > > > > >> > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > -- > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
Subject: Re: Cam Lobe wear
Date: Feb 13, 2007
From: "Monty Barrett Sr" <MONTY(at)bpaengines.com>
Sorry, Guys. Camshafts in Lycomings anc Continentals are NOT nitrided. The Lycoming is AISI 8620 and is carborized, about .030 deep. Don't know what the material is in TCM but it looks like and acts like a 1080 forging in which case it has enough carbon to harden without carborizing. Monty Barrett BPE, Inc. -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Monday, February 12, 2007 7:47 PM Subject: Re: Engines-List: Re: Cam Lobe wear What happens is a bit of rust or imperfection in the nitride layer causes a breakthrough to softer metal, on either cam or follower or both. Once that happens metal comes off quickly in relatively large particles..ones you can see. Oil analysis only detects metals at the microscopic size, that are vaporized in the spectrograph. Larger particles don't make it from the bottom of the sump, typically. My cam disintegrated, and luckily I was cutting the filter and saw the metal, and had to pull the oil pump for the AD on that and found it badly scored from the metal, so it was tear down time. I kept the cam and lifters as examples. I got to buy a replacement crank, new cam and lifters, and a new prop hub out of that episode...not all because of the cam, but from what I found on teardown. The good part is new prop hub I bought in 2002 is exempt from the current AD just issued this year. One gets very intimate with the details when you are building an engine for a type certified plane that you plan to fly, and may eventually sell to someone else, who will have your name in the logbooks as the mechanic that authorized its return to service, and may sue you 20 years later because it quit on them, even though they are 8 years and who knows how many hours past TBO. On 2/12/07, Gene Smith wrote: > > Kelly, > You seem like you have experience in this area and are knowledgeable about > the subject....Educate me about this, if an engine sets up unpickled for a > year, I understand from friends of mine that rust forms on the lobes, and > when started again, rust flakes off and contaminates the oil system, then > acts as pumice...Does this rust not show up on a spectrograph sample?..One > Tripacer owner neglected to change oil very often (if at all) and complained > of the engine not running right...I later saw the camshaft and there was > only "nubbins" left...I don't see how the valves functioned at all...I've > said this before, so will use this opportunity to mention it again, the > cheapest thing you can buy for your engine is OIL, and change it often...I > know the book says change at 50 hours, but I take a good look at mine at 25 > hours and if it exhibits the slightest darkness, then out it goes...One step > further, I use a 50/50 mix of Aeroshell and Mobil-I 15/w50, and after 1500 > hours, have had no problems at all...I do not advocate any of you out there > to use this mixture, especially certified aircraft...It is a personal thing > with me..........Kelly, thanks for your inputs...............CHEERS!!!! > > Gene Smith > RV-4 > > > ----- Original Message ----- > From: "Kelly McMullen" <apilot2(at)gmail.com> > To: > Sent: Monday, February 12, 2007 3:23 PM > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > Disagree on the oil analysis. Cam and lifters spall off relatively > > large chunks of metal, that are not microscopic and never burned in > > the spectrograph. You may see slightly elevated iron, but nothing > > startling, but you will see specks of iron in the oil filter. Went > > through this on my own IO-360 in 2001. > > KM, > > A&P/IA > > > > On 2/12/07, Gene Smith wrote: > > > > > > Yes, remove a cylinder and use a strong bright light and look up in > > > there...I removed #2, and you can see the lobes...The other choice (and > the > > > best) is to buy one of the oil analysis kits (around $10) and send off a > > > sample of your oil, and through a Spectroanalysis system (S.O.A.P.) they > can > > > tell you which component is wearing excessively by the type and amount > of > > > metal in your oil...As you know the different internal parts of your > engine > > > has a different type of metal...i.e: bearings, crankshaft journals, > valve > > > guides, cam lobes and etc. > > > > > > Interesting thing here as to the importance of this test, the USAF takes > a > > > S.O.A.P. sample after each flight of a Jet Fighter, (esp. if it is > single > > > engine) and the aircraft will not be released for the next mission until > the > > > analysis is complete and deemed safe......................Hope this > > > helps...Good luck.............................CHEERS!!!! > > > > > > Gene Smith > > > RV-4 > > > > > > > > > > > > ----- Original Message ----- > > > From: "Gary Casey" <glcasey(at)adelphia.net> > > > To: > > > Sent: Monday, February 12, 2007 7:45 AM > > > Subject: Engines-List: Re: Cam Lobe wear > > > > > > > > > > > > > > Dan, > > > > Yes, a compression test will not indicate that you have a problem > > > > with the cam. If it is really bad a cranking compression > > > > ("differential" compression test) might show the problem. Crank the > > > > engine with the mags and fuel off and note the difference between > > > > compression strokes - it is quite easy to tell if one cylinder is > > > > really low. You can pull the valve covers and measure the valve lift > > > > and that is one way to get a reasonable picture of cam lobe wear. > > > > You have to be careful about the hydraulic lifters as if one is > > > > collapsed you won't get an accurate measurement, but I don't know how > > > > to accommodate that, I'm afraid. From what I've heard, by the time > > > > the engine is running rough and is low on power the lobe will be > > > > essentially wiped off, making this method very effective - and it > > > > only takes a few minutes. I've used a simple steel scale, but a dial > > > > indicator would be more accurate. However, if you want to get a real > > > > look at the cam lobes the only way is to remove a cylinder - I'm told > > > > that on a 4-cylinder you can remove just one and get a peak at all > > > > the lobes, but I've never tried. Removing a cylinder isn't a huge > > > > deal, but it is a pain. It might take a day's labor to get it apart, > > > > inspected and put all back together. If the engine had no symptoms > > > > and looking in the valve covers showed no obvious problem, but showed > > > > metal in the filter then one has to look inside. With metal in the > > > > filter something is going to have to come apart anyway. > > > > > > > > Gary Casey > > > > > > > > > > Hi Gary, > > > > > > > > > > Some long time ago, you wrote the quote below. > > > > > > > > > > I am trying to find the cause of rough running in a Lyc O360A4M > > > > > that has > > > > > good compression, good mags, good timing. It has about 1400 smoh > over > > > > > about 12 years. There were times during those years in which it > > > > > sat for > > > > > over a year at a time. Also, for most of that time, the oil cooler > > > > > hoses were connected wrong so the oil ran quite hot. > > > > > > > > > > How can I prove that there is or isn't excessive cam lobe wear > without > > > > > tearing it all down?? > > > > > > > > > > Thanks, > > > > > > > > > > Dan > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: "William Becker" <wbecker(at)centurytel.net>
Subject: Re: Cam Lobe wear
Date: Feb 13, 2007
Gene, I'm no oil expert by any means, but I read a column by Ben Visser in General Aviation News www.generalaviationnews.com , he is an oil and fuel expert. Ben says that automotive oils use detergents and aviation oils use ashless dispersants. Both are for keeping the engine clean, but the detergents can cause carbon in aircraft engines, which could cause preignition. Might be a reason not to use an automotive oil, even a great one like Mobile 1 in aircraft. You can email Ben, maybe he could give his opinion, visser(at)GeneralAviationNews.com By the way I used the aircraft Mobile 1 for years in a banner tow aircraft, and it went past TBO, never had a cylinder off. Now I use AeroShell 15/50 semisynthetic Bill Becker. ----- Original Message ----- From: "Gene Smith" <esmith6(at)satx.rr.com> Sent: Monday, February 12, 2007 10:50 PM Subject: Re: Engines-List: Re: Cam Lobe wear > > Bill B., > I am not familiar with that oil, and did not know it was 50% synthetic, > but > thanks for the info, I certainly will investigate the Aeroshell...I get > the > Mobil I for $4.00 a quart...Is there a significant difference in price, > not > that it makes much difference when you are dealing with an aircraft > engine, > you always want the best...I am reluctant to say this, but with all the > fraud and lying going on in almost all aspects of our lives now days, I > know > for sure I'm getting 50% synthetic when I measure and mix it myself...In > no > way am I accusing Shell or any other aspect of aviation of wrong doing...I > run Mobil I in everything I have, including the lawn mower...I have one > auto > that the manufacturer requires it...Another reason I use the Aeroshell in > the aircraft mixture is because I'm not sure Mobil I has enough detergent, > otherwise, I would use 100% Mobil I which is 100% synthetic..That is one > slick stuff.......Thanks for the info......................CHEERS!!!! > > > ----- Original Message ----- > From: "William Becker" <wbecker(at)centurytel.net> > To: > Sent: Monday, February 12, 2007 9:20 PM > Subject: Re: Engines-List: Re: Cam Lobe wear > > > >> >> Why not just use Aeroshell 15/50, which is 50% synthetic ? Bill B >> ----- Original Message ----- >> From: "Gene Smith" <esmith6(at)satx.rr.com> >> To: >> Sent: Monday, February 12, 2007 6:54 PM >> Subject: Re: Engines-List: Re: Cam Lobe wear >> >> >> > >> > Kelly, >> > You seem like you have experience in this area and are knowledgeable > about >> > the subject....Educate me about this, if an engine sets up unpickled >> > for > a >> > year, I understand from friends of mine that rust forms on the lobes, > and >> > when started again, rust flakes off and contaminates the oil system, > then >> > acts as pumice...Does this rust not show up on a spectrograph > sample?..One >> > Tripacer owner neglected to change oil very often (if at all) and >> > complained >> > of the engine not running right...I later saw the camshaft and there >> > was >> > only "nubbins" left...I don't see how the valves functioned at > all...I've >> > said this before, so will use this opportunity to mention it again, the >> > cheapest thing you can buy for your engine is OIL, and change it > often...I >> > know the book says change at 50 hours, but I take a good look at mine >> > at >> > 25 >> > hours and if it exhibits the slightest darkness, then out it goes...One >> > step >> > further, I use a 50/50 mix of Aeroshell and Mobil-I 15/w50, and after > 1500 >> > hours, have had no problems at all...I do not advocate any of you out >> > there >> > to use this mixture, especially certified aircraft...It is a personal >> > thing >> > with me..........Kelly, thanks for your inputs...............CHEERS!!!! >> > >> > Gene Smith >> > RV-4 >> > >> > >> > ----- Original Message ----- >> > From: "Kelly McMullen" <apilot2(at)gmail.com> >> > To: >> > Sent: Monday, February 12, 2007 3:23 PM >> > Subject: Re: Engines-List: Re: Cam Lobe wear >> > >> > > >> >> >> >> Disagree on the oil analysis. Cam and lifters spall off relatively >> >> large chunks of metal, that are not microscopic and never burned in >> >> the spectrograph. You may see slightly elevated iron, but nothing >> >> startling, but you will see specks of iron in the oil filter. Went >> >> through this on my own IO-360 in 2001. >> >> KM, >> >> A&P/IA >> >> >> >> On 2/12/07, Gene Smith wrote: > >> >> > >> >> > Yes, remove a cylinder and use a strong bright light and look up in >> >> > there...I removed #2, and you can see the lobes...The other choice > (and >> > the >> >> > best) is to buy one of the oil analysis kits (around $10) and send > off >> >> > a >> >> > sample of your oil, and through a Spectroanalysis system (S.O.A.P.) >> >> > they >> > can >> >> > tell you which component is wearing excessively by the type and > amount >> > of >> >> > metal in your oil...As you know the different internal parts of your >> > engine >> >> > has a different type of metal...i.e: bearings, crankshaft journals, >> > valve >> >> > guides, cam lobes and etc. >> >> > >> >> > Interesting thing here as to the importance of this test, the USAF >> >> > takes >> > a >> >> > S.O.A.P. sample after each flight of a Jet Fighter, (esp. if it is >> > single >> >> > engine) and the aircraft will not be released for the next mission >> >> > until >> > the >> >> > analysis is complete and deemed safe......................Hope this >> >> > helps...Good luck.............................CHEERS!!!! >> >> > >> >> > Gene Smith >> >> > RV-4 >> >> > >> >> > >> >> > >> >> > ----- Original Message ----- >> >> > From: "Gary Casey" <glcasey(at)adelphia.net> >> >> > To: >> >> > Sent: Monday, February 12, 2007 7:45 AM >> >> > Subject: Engines-List: Re: Cam Lobe wear >> >> > >> >> > > >> >> > > >> >> > > Dan, >> >> > > Yes, a compression test will not indicate that you have a problem >> >> > > with the cam. If it is really bad a cranking compression >> >> > > ("differential" compression test) might show the problem. Crank > the >> >> > > engine with the mags and fuel off and note the difference between >> >> > > compression strokes - it is quite easy to tell if one cylinder is >> >> > > really low. You can pull the valve covers and measure the valve > lift >> >> > > and that is one way to get a reasonable picture of cam lobe wear. >> >> > > You have to be careful about the hydraulic lifters as if one is >> >> > > collapsed you won't get an accurate measurement, but I don't know > how >> >> > > to accommodate that, I'm afraid. From what I've heard, by the >> >> > > time >> >> > > the engine is running rough and is low on power the lobe will be >> >> > > essentially wiped off, making this method very effective - and it >> >> > > only takes a few minutes. I've used a simple steel scale, but a > dial >> >> > > indicator would be more accurate. However, if you want to get a > real >> >> > > look at the cam lobes the only way is to remove a cylinder - I'm > told >> >> > > that on a 4-cylinder you can remove just one and get a peak at all >> >> > > the lobes, but I've never tried. Removing a cylinder isn't a huge >> >> > > deal, but it is a pain. It might take a day's labor to get it > apart, >> >> > > inspected and put all back together. If the engine had no >> >> > > symptoms >> >> > > and looking in the valve covers showed no obvious problem, but > showed >> >> > > metal in the filter then one has to look inside. With metal in >> >> > > the >> >> > > filter something is going to have to come apart anyway. >> >> > > >> >> > > Gary Casey >> >> > > > >> >> > > > Hi Gary, >> >> > > > >> >> > > > Some long time ago, you wrote the quote below. >> >> > > > >> >> > > > I am trying to find the cause of rough running in a Lyc O360A4M >> >> > > > that has >> >> > > > good compression, good mags, good timing. It has about 1400 >> >> > > > smoh >> > over >> >> > > > about 12 years. There were times during those years in which it >> >> > > > sat for >> >> > > > over a year at a time. Also, for most of that time, the oil > cooler >> >> > > > hoses were connected wrong so the oil ran quite hot. >> >> > > > >> >> > > > How can I prove that there is or isn't excessive cam lobe wear >> > without >> >> > > > tearing it all down?? >> >> > > > >> >> > > > Thanks, >> >> > > > >> >> > > > Dan >> >> > > >> >> > > >> >> > > >> >> > > >> >> > >> >> > >> >> > >> >> > >> >> > >> >> > >> >> >> >> >> >> >> > >> > >> > >> > >> > >> > >> > >> > >> > -- >> > >> >> >> >> > > > -- > ________________________________________________________________________________
From: "jfs" <jfs(at)wildblue.net>
Subject: Re: Cam Lobe wear
Date: Feb 13, 2007
I asked my lil' brother for his take on this thread. His response follows: "Some of these guys are really misguided on many things, and some of them appear to be playing alchemist by mixing on their own volition. This is a strict no-no for many reasons. No time this morning for a full response, but a few points: Mobil 1 is an automotive oil, not approved for any Lyc or Continental as every other automotive oil is not... they contain detergents which can foul spark plugs in aircraft engines, particularly. the bottom plug. This is why only ashless oils are recommended, like Exxon Elite or the Aeroshell M/G. There is only one exception I can think of where Mobil 1 is used, in fact the only oil recommended... the Mooney Porsche, which the Germans at Porsche recommended only 1 oil for... 2 different viscosities of M1 depending on the ambient temp. I have heard of folks using M1 or someone else's auto oil in a Lycoming or Continental... all I can say is that they are fools and in violation of the OEM's, all of whom recommend only aviation oils. Aircraft engines are run under relatively slow speed, steady speed conditions for hours at a time... perfect conditions for deposits to form on spark plugs, Using detergent auto oils is therefore a safety of flight issue, and therefore the reason only ashless dispersant oils are approved. There is no better wear protection oil in the marketplace than Mobil 1... one of the reasons it is used by so many NASCAR teams and in F1, IRL, LeMans and so many other race classes. ExxonMobil has run it a million miles in a BMW under severe conditions... miniscule wear and an engine that was super clean at test end. The Mobil 1 that the writer below is probably referring to was Mobil AV 1, not Mobil 1. It was removed from the market many years ago, but the press and some of the trade rags got it way overblown w/ mistruths. It worked wonderfully in Lycomings and most Continentals, but when flown infrequently in certain big bore Continentals, there were a few ring sticking incidents. This can occur with all oils when moisture and infrequent flying get together, esp at altitude where some of the high flyers have to operate at richer mixtures to keep things cool. Avgas has a lot of lead, and the extra lead at rich mixture settings, and moisture get together to form a lead paste. This is the stuff that can stick ring/s or accumulate in props (which are when you think of it, perfect centrifuges) I saw a ton of engines flown to TBO that operated on Mobil AV1... that thing got real political and emotional. Mobil ended up paying bogus claims... we saw falsified logbooks etc... it was ugly, what some pilots will do to get $$$ out of any big pocket supplier. I hate lawyers and anybody related to one. There are still a number of pilots using Mobil AV1 with great satisfaction, altho' it was removed from the market many years ago (some loaded up on supply near the end) Believe me, when flown under the right conditions, you can't believe how clean those engines were. Go into the Smithsonian Air & Space Museum sometime, look up at the Voyager and notice the Mobil AV 1 decal... that around the world, non-stop flight used only Mobil AV1. Again, a good oil that got a bad rap... The reason ExxonMobil and Shell use partial synthetics (again, ashless) for their premium offerings is that the mineral oil portion has good natural "solvency" for keeping unwanted material in fine suspension, to be later drained out during the oil change. The synthetic portion gives the low temp performance and the high temp thermal and oxidative stability plus great wear protection... the additives used are key in enhancing the performance, especially w.r.t. wear & anti-rust performance One last comment about the guy who mixes... don't, especially an automotive with an aircraft oil. Your friends seem to have no idea what an oil like Exxon Elite has to go through... for starters, a series of lab tests... if successful (reviewed by the SAE Technical Committee 8 (chaired by the USN)), then a 150 hour endurance test (a real engine (we ran a Lyc TIO-540J2BD, a Piper Chieftain powerplant), run in a test cell under a variety of climb. descent and cruise profiles). If you get through that , you go to a 500 hour flight eval in 2 different engines. We chose the 2 most difficult, higher temp T/C engines... the Lyc previously mentioned & for the Continental, the TSIO520-BCE (used in a Cessna 402). All engines are disassembled and pre-measured for wear, then flown (both in test cell and on wing), then disassembled again and inspected/post measured for wear... all oil wetted parts... cams, valve guides, crank, cylinders, pistons, bearings etc... The engines are also sludge & deposit rated, so that in addition to wear performance, the oil needs to demonstrate excellent cleanliness. This rigor of approval is exactly why ExxonMobil's, Shell's, Phillip's etc stance on using additives of any kind is the way it is... one simply can't test all the possible combinations of "mouse milk" additives out there. It is usually wasted money spent. Stick to a great oil like Elite and be done with it. We look at a ton of cams that have been flown to TBO, and with Elite especially they look good with very minimal wear. The key is to fly as regular as possible, and use an oil with the highest level of rust protection available... these are most always the multi-grades, and among those, the Elite really stands out (we designed it that way, as statistics show that the average pilot in the US flies less than ~50 hours per year. We have a lot of data to back up this claim, both rust and wear protection is unsurpassed with Elite. You don't need to pass this along, as in re-reading it sounds like a commercial, but it's my life, and as an Engineer, I've seen too much data and too many engines. Can I go to work now?" ----- Original Message ----- From: "Kelly McMullen" <apilot2(at)gmail.com> Sent: Monday, February 12, 2007 10:28 PM Subject: Re: Engines-List: Re: Cam Lobe wear > > Don't let that Mobil 1 get anywhere near the airport. There was a big > class action and AD against Mobil 1 aircraft oil, lots of folks didn't > get the full cost of repairing damage that oil caused to engines, > props, governors. Exxon Elite or AeroShell 15-50 are both semi > synthetic. Both around 50-55 a case on sale. Exxon does on-line sale > for every major aviation event like SnF and OSH and AOPA Expo with > rebate of some sort to reach that price. They pay shipping(drop > shipped from closest distributor). > > On 2/12/07, Gene Smith wrote: ... .. . JF Schaefer, Sr. ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Re: Cam Lobe wear
Date: Feb 13, 2007
I know one guy who drops a bit of Aeroshell semi synthetic into his car a couple of hundred miles before an oil change. He swears it cleans out any sludge in his engine. Noel > -----Original Message----- > From: owner-engines-list-server(at)matronics.com > [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of > William Becker > Sent: Tuesday, February 13, 2007 4:23 PM > To: engines-list(at)matronics.com > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > Gene, > I'm no oil expert by any means, but I read a column by > Ben Visser in > General Aviation News www.generalaviationnews.com , he is an > oil and fuel > expert. Ben says that automotive oils use detergents and > aviation oils use > ashless dispersants. Both are for keeping the engine clean, but the > detergents can cause carbon in aircraft engines, which could cause > preignition. Might be a reason not to use an automotive oil, > even a great > one like Mobile 1 in aircraft. You can email Ben, maybe he > could give his > opinion, > visser(at)GeneralAviationNews.com > By the way I used the aircraft Mobile 1 for years in a banner > tow aircraft, > and it went past TBO, never had a cylinder off. Now I use > AeroShell 15/50 > semisynthetic > Bill Becker. > > ----- Original Message ----- > From: "Gene Smith" <esmith6(at)satx.rr.com> > To: > Sent: Monday, February 12, 2007 10:50 PM > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > > Bill B., > > I am not familiar with that oil, and did not know it was > 50% synthetic, > > but > > thanks for the info, I certainly will investigate the > Aeroshell...I get > > the > > Mobil I for $4.00 a quart...Is there a significant > difference in price, > > not > > that it makes much difference when you are dealing with an aircraft > > engine, > > you always want the best...I am reluctant to say this, but > with all the > > fraud and lying going on in almost all aspects of our lives > now days, I > > know > > for sure I'm getting 50% synthetic when I measure and mix > it myself...In > > no > > way am I accusing Shell or any other aspect of aviation of > wrong doing...I > > run Mobil I in everything I have, including the lawn > mower...I have one > > auto > > that the manufacturer requires it...Another reason I use > the Aeroshell in > > the aircraft mixture is because I'm not sure Mobil I has > enough detergent, > > otherwise, I would use 100% Mobil I which is 100% > synthetic..That is one > > slick stuff.......Thanks for the > info......................CHEERS!!!! > > > > > > > > ----- Original Message ----- > > From: "William Becker" <wbecker(at)centurytel.net> > > To: > > Sent: Monday, February 12, 2007 9:20 PM > > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > > >> > >> Why not just use Aeroshell 15/50, which is 50% synthetic ? > Bill B > >> ----- Original Message ----- > >> From: "Gene Smith" <esmith6(at)satx.rr.com> > >> To: > >> Sent: Monday, February 12, 2007 6:54 PM > >> Subject: Re: Engines-List: Re: Cam Lobe wear > >> > >> > > >> > > >> > Kelly, > >> > You seem like you have experience in this area and are > knowledgeable > > about > >> > the subject....Educate me about this, if an engine sets > up unpickled > >> > for > > a > >> > year, I understand from friends of mine that rust forms > on the lobes, > > and > >> > when started again, rust flakes off and contaminates the > oil system, > > then > >> > acts as pumice...Does this rust not show up on a spectrograph > > sample?..One > >> > Tripacer owner neglected to change oil very often (if at all) and > >> > complained > >> > of the engine not running right...I later saw the > camshaft and there > >> > was > >> > only "nubbins" left...I don't see how the valves functioned at > > all...I've > >> > said this before, so will use this opportunity to > mention it again, the > >> > cheapest thing you can buy for your engine is OIL, and change it > > often...I > >> > know the book says change at 50 hours, but I take a good > look at mine > >> > at > >> > 25 > >> > hours and if it exhibits the slightest darkness, then > out it goes...One > >> > step > >> > further, I use a 50/50 mix of Aeroshell and Mobil-I > 15/w50, and after > > 1500 > >> > hours, have had no problems at all...I do not advocate > any of you out > >> > there > >> > to use this mixture, especially certified aircraft...It > is a personal > >> > thing > >> > with me..........Kelly, thanks for your > inputs...............CHEERS!!!! > >> > > >> > Gene Smith > >> > RV-4 > >> > > >> > > >> > ----- Original Message ----- > >> > From: "Kelly McMullen" <apilot2(at)gmail.com> > >> > To: > >> > Sent: Monday, February 12, 2007 3:23 PM > >> > Subject: Re: Engines-List: Re: Cam Lobe wear > >> > > >> > > > > >> >> > >> >> Disagree on the oil analysis. Cam and lifters spall off > relatively > >> >> large chunks of metal, that are not microscopic and > never burned in > >> >> the spectrograph. You may see slightly elevated iron, > but nothing > >> >> startling, but you will see specks of iron in the oil > filter. Went > >> >> through this on my own IO-360 in 2001. > >> >> KM, > >> >> A&P/IA > >> >> > >> >> On 2/12/07, Gene Smith wrote: > > > >> >> > > >> >> > Yes, remove a cylinder and use a strong bright light > and look up in > >> >> > there...I removed #2, and you can see the lobes...The > other choice > > (and > >> > the > >> >> > best) is to buy one of the oil analysis kits (around > $10) and send > > off > >> >> > a > >> >> > sample of your oil, and through a Spectroanalysis > system (S.O.A.P.) > >> >> > they > >> > can > >> >> > tell you which component is wearing excessively by > the type and > > amount > >> > of > >> >> > metal in your oil...As you know the different > internal parts of your > >> > engine > >> >> > has a different type of metal...i.e: bearings, > crankshaft journals, > >> > valve > >> >> > guides, cam lobes and etc. > >> >> > > >> >> > Interesting thing here as to the importance of this > test, the USAF > >> >> > takes > >> > a > >> >> > S.O.A.P. sample after each flight of a Jet Fighter, > (esp. if it is > >> > single > >> >> > engine) and the aircraft will not be released for the > next mission > >> >> > until > >> > the > >> >> > analysis is complete and deemed > safe......................Hope this > >> >> > helps...Good luck.............................CHEERS!!!! > >> >> > > >> >> > Gene Smith > >> >> > RV-4 > >> >> > > >> >> > > >> >> > > >> >> > ----- Original Message ----- > >> >> > From: "Gary Casey" <glcasey(at)adelphia.net> > >> >> > To: > >> >> > Sent: Monday, February 12, 2007 7:45 AM > >> >> > Subject: Engines-List: Re: Cam Lobe wear > >> >> > > >> >> > > > > >> >> > > > >> >> > > Dan, > >> >> > > Yes, a compression test will not indicate that you > have a problem > >> >> > > with the cam. If it is really bad a cranking compression > >> >> > > ("differential" compression test) might show the > problem. Crank > > the > >> >> > > engine with the mags and fuel off and note the > difference between > >> >> > > compression strokes - it is quite easy to tell if > one cylinder is > >> >> > > really low. You can pull the valve covers and > measure the valve > > lift > >> >> > > and that is one way to get a reasonable picture of > cam lobe wear. > >> >> > > You have to be careful about the hydraulic lifters > as if one is > >> >> > > collapsed you won't get an accurate measurement, > but I don't know > > how > >> >> > > to accommodate that, I'm afraid. From what I've > heard, by the > >> >> > > time > >> >> > > the engine is running rough and is low on power the > lobe will be > >> >> > > essentially wiped off, making this method very > effective - and it > >> >> > > only takes a few minutes. I've used a simple steel > scale, but a > > dial > >> >> > > indicator would be more accurate. However, if you > want to get a > > real > >> >> > > look at the cam lobes the only way is to remove a > cylinder - I'm > > told > >> >> > > that on a 4-cylinder you can remove just one and > get a peak at all > >> >> > > the lobes, but I've never tried. Removing a > cylinder isn't a huge > >> >> > > deal, but it is a pain. It might take a day's > labor to get it > > apart, > >> >> > > inspected and put all back together. If the engine had no > >> >> > > symptoms > >> >> > > and looking in the valve covers showed no obvious > problem, but > > showed > >> >> > > metal in the filter then one has to look inside. > With metal in > >> >> > > the > >> >> > > filter something is going to have to come apart anyway. > >> >> > > > >> >> > > Gary Casey > >> >> > > > > >> >> > > > Hi Gary, > >> >> > > > > >> >> > > > Some long time ago, you wrote the quote below. > >> >> > > > > >> >> > > > I am trying to find the cause of rough running in > a Lyc O360A4M > >> >> > > > that has > >> >> > > > good compression, good mags, good timing. It has > about 1400 > >> >> > > > smoh > >> > over > >> >> > > > about 12 years. There were times during those > years in which it > >> >> > > > sat for > >> >> > > > over a year at a time. Also, for most of that > time, the oil > > cooler > >> >> > > > hoses were connected wrong so the oil ran quite hot. > >> >> > > > > >> >> > > > How can I prove that there is or isn't excessive > cam lobe wear > >> > without > >> >> > > > tearing it all down?? > >> >> > > > > >> >> > > > Thanks, > >> >> > > > > >> >> > > > Dan > >> >> > > > >> >> > > > >> >> > > > >> >> > > > >> >> > > >> >> > > >> >> > > >> >> > > >> >> > > >> >> > > >> >> > >> >> > >> >> > >> > > >> > > >> > > >> > > >> > > >> > > >> > > >> > > >> > -- > >> > > >> > >> > >> > >> > > > > > > > > > > > > > > > > > > -- > > > > > > > ________________________________________________________________________________
From: "Red Hamilton" <redswing(at)mcn.org>
Subject: Re: Cam Lobe wear
Date: Feb 13, 2007
Thanks for the straight scoop Monty. Red Hamilton ----- Original Message ----- From: Monty Barrett Sr To: engines-list(at)matronics.com Sent: Tuesday, February 13, 2007 8:37 AM Subject: RE: Engines-List: Re: Cam Lobe wear Sorry, Guys. Camshafts in Lycomings and Continentals are NOT nitrided. The Lycoming is AISI 8620 and is carborized, about .030 deep. Don't know what the material is in TCM but it looks like and acts like a 1080 forging in which case it has enough carbon to harden without carborizing. Monty Barrett BPE, Inc. -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Monday, February 12, 2007 7:47 PM To: engines-list(at)matronics.com Subject: Re: Engines-List: Re: Cam Lobe wear What happens is a bit of rust or imperfection in the nitride layer causes a breakthrough to softer metal, on either cam or follower or both. Once that happens metal comes off quickly in relatively large particles..ones you can see. Oil analysis only detects metals at the microscopic size, that are vaporized in the spectrograph. Larger particles don't make it from the bottom of the sump, typically. My cam disintegrated, and luckily I was cutting the filter and saw the metal, and had to pull the oil pump for the AD on that and found it badly scored from the metal, so it was tear down time. I kept the cam and lifters as examples. I got to buy a replacement crank, new cam and lifters, and a new prop hub out of that episode...not all because of the cam, but from what I found on teardown. The good part is new prop hub I bought in 2002 is exempt from the current AD just issued this year. One gets very intimate with the details when you are building an engine for a type certified plane that you plan to fly, and may eventually sell to someone else, who will have your name in the logbooks as the mechanic that authorized its return to service, and may sue you 20 years later because it quit on them, even though they are 8 years and who knows how many hours past TBO. On 2/12/07, Gene Smith wrote: > > Kelly, > You seem like you have experience in this area and are knowledgeable about > the subject....Educate me about this, if an engine sets up unpickled for a > year, I understand from friends of mine that rust forms on the lobes, and > when started again, rust flakes off and contaminates the oil system, then > acts as pumice...Does this rust not show up on a spectrograph sample?..One > Tripacer owner neglected to change oil very often (if at all) and complained > of the engine not running right...I later saw the camshaft and there was > only "nubbins" left...I don't see how the valves functioned at all...I've > said this before, so will use this opportunity to mention it again, the > cheapest thing you can buy for your engine is OIL, and change it often...I > know the book says change at 50 hours, but I take a good look at mine at 25 > hours and if it exhibits the slightest darkness, then out it goes...One step > further, I use a 50/50 mix of Aeroshell and Mobil-I 15/w50, and after 1500 > hours, have had no problems at all...I do not advocate any of you out there > to use this mixture, especially certified aircraft...It is a personal thing > with me..........Kelly, thanks for your inputs...............CHEERS!!!! > > Gene Smith > RV-4 > > > ----- Original Message ----- > From: "Kelly McMullen" <apilot2(at)gmail.com> > To: > Sent: Monday, February 12, 2007 3:23 PM > Subject: Re: Engines-List: Re: Cam Lobe wear > > > > > > Disagree on the oil analysis. Cam and lifters spall off relatively > > large chunks of metal, that are not microscopic and never burned in > > the spectrograph. You may see slightly elevated iron, but nothing > > startling, but you will see specks of iron in the oil filter. Went > > through this on my own IO-360 in 2001. > > KM, > > A&P/IA > > > > On 2/12/07, Gene Smith wrote: > > > > > > Yes, remove a cylinder and use a strong bright light and look up in > > > there...I removed #2, and you can see the lobes...The other choice (and > the > > > best) is to buy one of the oil analysis kits (around $10) and send off a > > > sample of your oil, and through a Spectroanalysis system (S.O.A.P.) they > can > > > tell you which component is wearing excessively by the type and amount > of > > > metal in your oil...As you know the different internal parts of your > engine > > > has a different type of metal...i.e: bearings, crankshaft journals, > valve > > > guides, cam lobes and etc. > > > > > > Interesting thing here as to the importance of this test, the USAF takes > a > > > S.O.A.P. sample after each flight of a Jet Fighter, (esp. if it is > single > > > engine) and the aircraft will not be released for the next mission until > the > > > analysis is complete and deemed safe......................Hope this > > > helps...Good luck.............................CHEERS!!!! > > > > > > Gene Smith > > > RV-4 > > > > > > > > > > > > ----- Original Message ----- > > > From: "Gary Casey" <glcasey(at)adelphia.net> > > > To: > > > Sent: Monday, February 12, 2007 7:45 AM > > > Subject: Engines-List: Re: Cam Lobe wear > > > > > > > > > > > > > > Dan, > > > > Yes, a compression test will not indicate that you have a problem > > > > with the cam. If it is really bad a cranking compression > > > > ("differential" compression test) might show the problem. Crank the > > > > engine with the mags and fuel off and note the difference between > > > > compression strokes - it is quite easy to tell if one cylinder is > > > > really low. You can pull the valve covers and measure the valve lift > > > > and that is one way to get a reasonable picture of cam lobe wear. > > > > You have to be careful about the hydraulic lifters as if one is > > > > collapsed you won't get an accurate measurement, but I don't know how > > > > to accommodate that, I'm afraid. From what I've heard, by the time > > > > the engine is running rough and is low on power the lobe will be > > > > essentially wiped off, making this method very effective - and it > > > > only takes a few minutes. I've used a simple steel scale, but a dial > > > > indicator would be more accurate. However, if you want to get a real > > > > look at the cam lobes the only way is to remove a cylinder - I'm told > > > > that on a 4-cylinder you can remove just one and get a peak at all > > > > the lobes, but I've never tried. Removing a cylinder isn't a huge > > > > deal, but it is a pain. It might take a day's labor to get it apart, > > > > inspected and put all back together. If the engine had no symptoms > > > > and looking in the valve covers showed no obvious problem, but showed > > > > metal in the filter then one has to look inside. With metal in the > > > > filter something is going to have to come apart anyway. > > > > > > > > Gary Casey > > > > > > > > > > Hi Gary, > > > > > > > > > > Some long time ago, you wrote the quote below. > > > > > > > > > > I am trying to find the cause of rough running in a Lyc O360A4M > > > > > that has > > > > > good compression, good mags, good timing. It has about 1400 smoh > over > > > > > about 12 years. There were times during those years in which it > > > > > sat for > > > > > over a year at a time. Also, for most of that time, the oil cooler > > > > > hoses were connected wrong so the oil ran quite hot. > > > > > > > > > > How can I prove that there is or isn't excessive cam lobe wear > without > > > > > tearing it all down?? > > > > > > > > > > Thanks, > > > > > > > > > > Dan > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > ________________________________________________________________________________
From: "Fergus Kyle" <VE3LVO(at)rac.ca>
Subject: Come on, ladies
Date: Feb 14, 2007
It's time to read the Matronics Rules of Engagement (again?). The last engines-list digest displays a thousand unneeded repeat lines, some messages repeating up to nine previous messages - each. Read what you write - first - then send. Ferg Kyle Europa A064 914 Classic ________________________________________________________________________________
Date: Feb 15, 2007
From: "DEAN PSIROPOULOS" <dean.psiropoulos(at)verizon.net>
Subject: Engines-lack of usage
I'm not sure that I actually heard an answer to the question posed the other day (feel free to kick me if I read right by it) so the real question still remains.... is an engine that has been sitting for a couple years in a hangar going to suffer from internal corrosion problems and have to be torn down before starting? How about a worst case scenario where a newly assembled engine is delivered to the tropics and stored in a hangar that is not climate controlled. The engine is pickled and plastic plugs have been installed in the openings but some of them don't seal very well and there are no dessicant plugs installed. Would a couple years under these conditions cause enough corrosion that the engine would have problems if one were to just fill it with oil and go fly it? What kind of problems would one expect? Is there any way to tell the extent of damage without major teardown or cylinder removal? What would you expect to see corroded inside (cam, rods, gears, crank) and would you recommend not running the engine before an internal inspection? Would there be a pre-start procedure you'd recommend before starting an engine that has been subjected to these conditions? Anybody done any testing of this sort and is there any data available on just how bad it gets? Would you trust such an engine not to fail in a short period of time if some unsuspecting pilot just put it on his airplane and flew it? What sort of failure mode would you expect and do you think the outcome would be catastrophic (engine destroyed)? Any words of wisdom here Monty Barrett (or anyone else with experience in this area)? Thanks. Dean Psiropoulos ________________________________________________________________________________
Date: Feb 15, 2007
From: "Bob" <rfg842(at)cox.net>
Subject: Costly mistake
Bought an aircraft, sight unseen, from Arizona with a Lyc 0 290 D2 wi th some 200 hours on a chrome major. After flying it for two years, could never get the oil consumption down so decided to give it a top. When the IA opened it up, found a bad cam, lots of internal rust and a $15,000 major. Don't know if Lyc is prone to these problems but will never trust another purchase without a good internal inspection. Would have saved me thousan ds. Bob, Wichita ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Engines-lack of usage
Date: Feb 15, 2007
I think a lot has to do with how the engines were mothballed for storage. Properly mothballed there should be no problems. Returning to service will not just be a matter of pouring in some oil and heading out to the great blue yonder. Cylinders should have had desiccant plugs and the base should have been filled with preservative oil. The oil must be drained the engine turned over with out the sparkplugs several times and then you can think about putting fresh oil in. Installing plugs, possibly mags, carbs etc and then there may, for a new engine, be a break in. Best thing is to check the MM for the engine and any return to use instructions that may have come with the engine. Pay particular attention to the Maintenance Manual if you mothball the engine later. Noel > -----Original Message----- > From: owner-engines-list-server(at)matronics.com > [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of > DEAN PSIROPOULOS > Sent: Thursday, February 15, 2007 2:53 AM > To: engines-list(at)matronics.com > Subject: Engines-List: Engines-lack of usage > > > > > I'm not sure that I actually heard an answer to the question > posed the other > day (feel free to kick me if I read right by it) so the real > question still > remains.... is an engine that has been sitting for a couple years in a > hangar going to suffer from internal corrosion problems and > have to be torn > down before starting? > > How about a worst case scenario where a newly assembled > engine is delivered > to the tropics and stored in a hangar that is not climate > controlled. The > engine is pickled and plastic plugs have been installed in > the openings but > some of them don't seal very well and there are no dessicant plugs > installed. Would a couple years under these conditions cause enough > corrosion that the engine would have problems if one were to > just fill it > with oil and go fly it? > > What kind of problems would one expect? > > Is there any way to tell the extent of damage without major > teardown or > cylinder removal? > > What would you expect to see corroded inside (cam, rods, > gears, crank) and > would you recommend not running the engine before an internal > inspection? > > Would there be a pre-start procedure you'd recommend before > starting an > engine that has been subjected to these conditions? > > Anybody done any testing of this sort and is there any data > available on > just how bad it gets? > > Would you trust such an engine not to fail in a short period > of time if some > unsuspecting pilot just put it on his airplane and flew it? > > What sort of failure mode would you expect and do you think > the outcome > would be catastrophic (engine destroyed)? > > Any words of wisdom here Monty Barrett (or anyone else with > experience in > this area)? Thanks. > > Dean Psiropoulos > > > > > > > > ________________________________________________________________________________
Date: Feb 15, 2007
From: JIM AITKEN <matrix02(at)shaw.ca>
Subject: Re: Engines-lack of usage
My comment is on the storage of an engine or an airplane or any machinery in an unventilated hanger or garage. If there is no provision for vents under the ceiling or roof moisture collects from the dinural temperature variations and corrosion is worse than leaving the item outside where the moisture will dissipate. A hangar with uninsulated steel siding and a dirt floor compounds the situation. I have seen airplanes in unventilated closed hangars dripping with condensation. The old wives tale that putting a car in a closed garage after washing it creates rusting is quite true. Domestic garages do not provide for any ventilation and the moisture does not dissipate allowing it to seep into crevasses and enhance corrosion. Jim Aitken ----- Original Message ----- From: DEAN PSIROPOULOS <dean.psiropoulos(at)verizon.net> Date: Thursday, February 15, 2007 0:23 am Subject: Engines-List: Engines-lack of usage > > I'm not sure that I actually heard an answer to the question posed > the other > day (feel free to kick me if I read right by it) so the real > question still > remains.... is an engine that has been sitting for a couple years > in a > hangar going to suffer from internal corrosion problems and have > to be torn > down before starting? > > How about a worst case scenario where a newly assembled engine is > deliveredto the tropics and stored in a hangar that is not climate > controlled. The > engine is pickled and plastic plugs have been installed in the > openings but > some of them don't seal very well and there are no dessicant plugs > installed. Would a couple years under these conditions cause enough > corrosion that the engine would have problems if one were to just > fill it > with oil and go fly it? > > What kind of problems would one expect? > > Is there any way to tell the extent of damage without major > teardown or > cylinder removal? > > What would you expect to see corroded inside (cam, rods, gears, > crank) and > would you recommend not running the engine before an internal > inspection? > > Would there be a pre-start procedure you'd recommend before > starting an > engine that has been subjected to these conditions? > > Anybody done any testing of this sort and is there any data > available on > just how bad it gets? > > Would you trust such an engine not to fail in a short period of > time if some > unsuspecting pilot just put it on his airplane and flew it? > > What sort of failure mode would you expect and do you think the > outcomewould be catastrophic (engine destroyed)? > > Any words of wisdom here Monty Barrett (or anyone else with > experience in > this area)? Thanks. > > Dean Psiropoulos > > > > > > > > > ________________________________________________________________________________
From: Hopperdhh(at)aol.com
Date: Feb 15, 2007
Subject: Re: Costly mistake
In a message dated 2/15/2007 10:15:21 AM Eastern Standard Time, rfg842(at)cox.net writes: Bought an aircraft, sight unseen, from Arizona with a Lyc 0 290 D2 with some 200 hours on a chrome major. After flying it for two years, could never get the oil consumption down so decided to give it a top. When the IA opened it up, found a bad cam, lots of internal rust and a $15,000 major. Don't know if Lyc is prone to these problems but will never trust another purchase without a good internal inspection. Would have saved me thousands. Bob, Wichita Bob, How bad was the oil consumption? I had a Grumman with chrome cylinders (O-235) that would use a quart in 4 to 6 hours. I took the cylinders off and had them honed. The engine had zero rust inside, it looked like new in fact. After putting new rings in it and breaking it in using the best information I could get from many web searches -- kept temps down, power up, etc. -- it was exactly the same! Chrome doesn't rust, but it may take 300 hours for the rings to seat. Maybe the rough pattern of the chrome surface holds the oil and the engine consumes oil even after the rings seat. My RV has Cerminil (c) cylinders and seems to be much better. Dan Hopper RV-7A ________________________________________________________________________________
From: "Butch" <kmodairy(at)centurytel.net>
Subject: Re: Costly mistake
Date: Feb 15, 2007
You guys are not makeing me feel very good. I have a Colt sitting in a hanger for a little over a year now, was a great running 235 may not be now. Anybody had one that has sat for a while and was not damaged ? (I hope) ----- Original Message ----- From: Hopperdhh(at)aol.com To: engines-list(at)matronics.com Sent: Thursday, February 15, 2007 1:47 PM Subject: Re: Engines-List: Costly mistake In a message dated 2/15/2007 10:15:21 AM Eastern Standard Time, rfg842(at)cox.net writes: Bought an aircraft, sight unseen, from Arizona with a Lyc 0 290 D2 with some 200 hours on a chrome major. After flying it for two years, could never get the oil consumption down so decided to give it a top. When the IA opened it up, found a bad cam, lots of internal rust and a $15,000 major. Don't know if Lyc is prone to these problems but will never trust another purchase without a good internal inspection. Would have saved me thousands. Bob, Wichita Bob, How bad was the oil consumption? I had a Grumman with chrome cylinders (O-235) that would use a quart in 4 to 6 hours. I took the cylinders off and had them honed. The engine had zero rust inside, it looked like new in fact. After putting new rings in it and breaking it in using the best information I could get from many web searches -- kept temps down, power up, etc. -- it was exactly the same! Chrome doesn't rust, but it may take 300 hours for the rings to seat. Maybe the rough pattern of the chrome surface holds the oil and the engine consumes oil even after the rings seat. My RV has Cerminil (c) cylinders and seems to be much better. Dan Hopper RV-7A ________________________________________________________________________________
From: "William Becker" <wbecker(at)centurytel.net>
Subject: Re: Costly mistake
Date: Feb 15, 2007
I bought a project airplane a few years ago. The engine was in a hanger about 1 1/2 years with no special care, didn't even have the plugs in it. When I got it home I put Aeoshell fluid 2F in it and rotated the whole engine around a couple times, put in dehydrator plugs, then it sat for 2 years while I rebuilt the airplane. It has been a great engine, now has over 300 hrs since I bought the project. I would never suggest treating an engine that way. I would always use Aeroshell fluid2F if an engine was to be stored for over 2 month or so. If you can run the engine, I would run it, drain the oil and put in the Aeroshell fluid2F then run it again and put it away. The big worry as far as I am concerned is the cam and lifters, they will not tolerate rust. You can remove a cylinder and look inside to verify that no rust is present, no need for a tear down. My 2 pennies. Bill Becker ----- Original Message ----- From: Butch To: engines-list(at)matronics.com Sent: Thursday, February 15, 2007 2:38 PM Subject: Re: Engines-List: Costly mistake You guys are not makeing me feel very good. I have a Colt sitting in a hanger for a little over a year now, was a great running 235 may not be now. Anybody had one that has sat for a while and was not damaged ? (I hope) ----- Original Message ----- From: Hopperdhh(at)aol.com To: engines-list(at)matronics.com Sent: Thursday, February 15, 2007 1:47 PM Subject: Re: Engines-List: Costly mistake In a message dated 2/15/2007 10:15:21 AM Eastern Standard Time, rfg842(at)cox.net writes: Bought an aircraft, sight unseen, from Arizona with a Lyc 0 290 D2 with some 200 hours on a chrome major. After flying it for two years, could never get the oil consumption down so decided to give it a top. When the IA opened it up, found a bad cam, lots of internal rust and a $15,000 major. Don't know if Lyc is prone to these problems but will never trust another purchase without a good internal inspection. Would have saved me thousands. Bob, Wichita Bob, How bad was the oil consumption? I had a Grumman with chrome cylinders (O-235) that would use a quart in 4 to 6 hours. I took the cylinders off and had them honed. The engine had zero rust inside, it looked like new in fact. After putting new rings in it and breaking it in using the best information I could get from many web searches -- kept temps down, power up, etc. -- it was exactly the same! Chrome doesn't rust, but it may take 300 hours for the rings to seat. Maybe the rough pattern of the chrome surface holds the oil and the engine consumes oil even after the rings seat. My RV has Cerminil (c) cylinders and seems to be much better. Dan Hopper RV-7A href="http://www.matronics.com/Navigator?Engines-List">http://www.matro nics.com/Navigator?Engines-List href="http://forums.matronics.com">http://forums.matronics.com ------------------------------------------------------------------------- ----- 1/18/2007 ________________________________________________________________________________
Subject: Costly mistake
Date: Feb 15, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
________________________________ From: Sent: Thursday, February 15, 2007 1:48 PM Subject: RE: Engines-List: Costly mistake You know one of the best preserving ideas I ever heard was to buy some cheap oil for your car and completly fill the crankcase...I.e drive out all the oil. When you get it half full turn it over slowly a couple of times, then finish filling it up. The fill up the cylinders as well if you have some scrap plugs , of course you will need to remove the rocker arms to keep the valves closed but that can't be too difficult. . No way it can rust now and you can use the oil in your car afterwards... Frank ________________________________ From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of William Becker Sent: Thursday, February 15, 2007 1:20 PM Subject: Re: Engines-List: Costly mistake I bought a project airplane a few years ago. The engine was in a hanger about 1 1/2 years with no special care, didn't even have the plugs in it. When I got it home I put Aeoshell fluid 2F in it and rotated the whole engine around a couple times, put in dehydrator plugs, then it sat for 2 years while I rebuilt the airplane. It has been a great engine, now has over 300 hrs since I bought the project. I would never suggest treating an engine that way. I would always use Aeroshell fluid2F if an engine was to be stored for over 2 month or so. If you can run the engine, I would run it, drain the oil and put in the Aeroshell fluid2F then run it again and put it away. The big worry as far as I am concerned is the cam and lifters, they will not tolerate rust. You can remove a cylinder and look inside to verify that no rust is present, no need for a tear down. My 2 pennies. Bill Becker ________________________________________________________________________________
From: "Archie" <archie97(at)earthlink.net>
Subject: Re: Costly mistake
Date: Feb 15, 2007
Do not feel too badly, Bob Some have been there, and others will be. Tough lesson learned. Archie ----- Original Message ----- From: Bob To: engines-list(at)matronics.com Sent: Thursday, February 15, 2007 10:13 AM Subject: Engines-List: Costly mistake Bought an aircraft, sight unseen, from Arizona with a Lyc 0 290 D2 with some 200 hours on a chrome major. After flying it for two years, could never get the oil consumption down so decided to give it a top. When the IA opened it up, found a bad cam, lots of internal rust and a $15,000 major. Don't know if Lyc is prone to these problems but will never trust another purchase without a good internal inspection. Would have saved me thousands. Bob, Wichita ________________________________________________________________________________
From: "jrc" <jrccea(at)bellsouth.net>
Subject: Re: Engines-lack of usage
Date: Feb 15, 2007
It takes about 2 hours to pull and replace a cylinder so you can look inside the engine. That's a good investment of time. ----- Original Message ----- From: "DEAN PSIROPOULOS" <dean.psiropoulos(at)verizon.net> Sent: Thursday, February 15, 2007 12:23 AM Subject: Engines-List: Engines-lack of usage > > > I'm not sure that I actually heard an answer to the question posed the > other > day (feel free to kick me if I read right by it) so the real question > still > remains.... is an engine that has been sitting for a couple years in a > hangar going to suffer from internal corrosion problems and have to be > torn > down before starting? ________________________________________________________________________________
From: "Dacha" <tstaley(at)centurytel.net>
Subject: Re: Costly mistake
Date: Feb 15, 2007
Any Soob drivers out there? What kind of oil consumption are you experiencing? Mine is about one quart for 3 hours. Also know of anyone in Missouri that can tune it up or rebuild one? LeRoy ________________________________________________________________________________
Date: Feb 15, 2007
From: Jeff Boatright <jboatri(at)emory.edu>
Subject: Re: Engines-lack of usage
It shouldn't even take that long. And I agree, it's an excellent investment of time. We had two off and inspected in a half hour: http://userwww.service.emory.edu/~jboatri/magicbus/engine_teardown.htm > >It takes about 2 hours to pull and replace a cylinder so you can >look inside the engine. That's a good investment of time. -- _____________________________________________________________ Jeffrey H. Boatright, PhD Associate Professor, Emory Eye Center, Atlanta, GA, USA Senior Editor, Molecular Vision, http://www.molvis.org/molvis mailto:jboatri(at)emory.edu ________________________________________________________________________________
From: "Wayne Sweet" <w_sweet(at)comcast.net>
Subject: Re: Costly mistake
Date: Feb 15, 2007
I thought since oil floats on water, the condensation will get "under" the oil and bingo, rust. Wayne ----- Original Message ----- From: Hinde, Frank George (Corvallis) To: engines-list(at)matronics.com Sent: Thursday, February 15, 2007 2:02 PM Subject: RE: Engines-List: Costly mistake ------------------------------------------------------------------------- ----- From: Sent: Thursday, February 15, 2007 1:48 PM To: 'engines-list(at)matronics.com' Subject: RE: Engines-List: Costly mistake You know one of the best preserving ideas I ever heard was to buy some cheap oil for your car and completly fill the crankcase...I.e drive out all the oil. When you get it half full turn it over slowly a couple of times, then finish filling it up. The fill up the cylinders as well if you have some scrap plugs , of course you will need to remove the rocker arms to keep the valves closed but that can't be too difficult. . No way it can rust now and you can use the oil in your car afterwards... Frank ------------------------------------------------------------------------- ----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of William Becker Sent: Thursday, February 15, 2007 1:20 PM To: engines-list(at)matronics.com Subject: Re: Engines-List: Costly mistake I bought a project airplane a few years ago. The engine was in a hanger about 1 1/2 years with no special care, didn't even have the plugs in it. When I got it home I put Aeoshell fluid 2F in it and rotated the whole engine around a couple times, put in dehydrator plugs, then it sat for 2 years while I rebuilt the airplane. It has been a great engine, now has over 300 hrs since I bought the project. I would never suggest treating an engine that way. I would always use Aeroshell fluid2F if an engine was to be stored for over 2 month or so. If you can run the engine, I would run it, drain the oil and put in the Aeroshell fluid2F then run it again and put it away. The big worry as far as I am concerned is the cam and lifters, they will not tolerate rust. You can remove a cylinder and look inside to verify that no rust is present, no need for a tear down. My 2 pennies. Bill Becker ________________________________________________________________________________
From: "William Becker" <wbecker(at)centurytel.net>
Subject: Re: Costly mistake
Date: Feb 15, 2007
Well then the water would be at the bottom of the sump, so no harm to the engine parts. Right? Bill B ----- Original Message ----- From: Wayne Sweet To: engines-list(at)matronics.com Sent: Thursday, February 15, 2007 6:20 PM Subject: Re: Engines-List: Costly mistake I thought since oil floats on water, the condensation will get "under" the oil and bingo, rust. Wayne ----- Original Message ----- From: Hinde, Frank George (Corvallis) To: engines-list(at)matronics.com Sent: Thursday, February 15, 2007 2:02 PM Subject: RE: Engines-List: Costly mistake ------------------------------------------------------------------------- --- From: Sent: Thursday, February 15, 2007 1:48 PM To: 'engines-list(at)matronics.com' Subject: RE: Engines-List: Costly mistake You know one of the best preserving ideas I ever heard was to buy some cheap oil for your car and completly fill the crankcase...I.e drive out all the oil. When you get it half full turn it over slowly a couple of times, then finish filling it up. The fill up the cylinders as well if you have some scrap plugs , of course you will need to remove the rocker arms to keep the valves closed but that can't be too difficult. . No way it can rust now and you can use the oil in your car afterwards... Frank ------------------------------------------------------------------------- --- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of William Becker Sent: Thursday, February 15, 2007 1:20 PM To: engines-list(at)matronics.com Subject: Re: Engines-List: Costly mistake I bought a project airplane a few years ago. The engine was in a hanger about 1 1/2 years with no special care, didn't even have the plugs in it. When I got it home I put Aeoshell fluid 2F in it and rotated the whole engine around a couple times, put in dehydrator plugs, then it sat for 2 years while I rebuilt the airplane. It has been a great engine, now has over 300 hrs since I bought the project. I would never suggest treating an engine that way. I would always use Aeroshell fluid2F if an engine was to be stored for over 2 month or so. If you can run the engine, I would run it, drain the oil and put in the Aeroshell fluid2F then run it again and put it away. The big worry as far as I am concerned is the cam and lifters, they will not tolerate rust. You can remove a cylinder and look inside to verify that no rust is present, no need for a tear down. My 2 pennies. Bill Becker href="http://www.matronics.com/Navigator?Engines-List">http://www.matro nics.com/Navigator?Engines-List href="http://forums.matronics.com">http://forums.matronics.com ------------------------------------------------------------------------- ----- 1/18/2007 ________________________________________________________________________________
Date: Feb 15, 2007
From: "Rick" <wingsdown(at)verizon.net>
Subject: Costly mistake
Say Leroy a quart in 3 hours is a sure sign that either it is blowing it out he breather or rings. Does it slow down after the first quart? Rick -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Dacha Sent: Thursday, February 15, 2007 3:35 PM Subject: Re: Engines-List: Costly mistake Any Soob drivers out there? What kind of oil consumption are you experiencing? Mine is about one quart for 3 hours. Also know of anyone in Missouri that can tune it up or rebuild one? LeRoy ________________________________________________________________________________
From: "Dacha" <tstaley(at)centurytel.net>
Subject: Re: Costly mistake
Date: Feb 15, 2007
No Rick it doesnt slow down on the consumption after the first quart. Doesnt seem to be blowing it out, bottom of the plane stays pretty clean. Guess it is the rings but the compresion isnt too low, around 160-170. ________________________________________________________________________________
Date: Feb 15, 2007
From: john koning <fltrbg(at)yahoo.com>
Subject: Costly mistake
Taken one step further,I bought my A-75 flipped upside down, the crankcase filled through the drain plug, the cylinders filled through the bottom plugs,the exhaust ports filled,removed the carb and filled the intake spider.The rockers can then stay on,rocker boxes also fill up with oil,guides and all are submurged.Just remember to plug the crancase vent. John. "Hinde, Frank George (Corvallis)" wrote: --------------------------------- From: Sent: Thursday, February 15, 2007 1:48 PM Subject: RE: Engines-List: Costly mistake You know one of the best preserving ideas I ever heard was to buy some cheap oil for your car and completly fill the crankcase...I.e drive out all the oil. When you get it half full turn it over slowly a couple of times, then finish filling it up. The fill up the cylinders as well if you have some scrap plugs , of course you will need to remove the rocker arms to keep the valves closed but that can't be too difficult. . No way it can rust now and you can use the oil in your car afterwards... Frank --------------------------------- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of William Becker Sent: Thursday, February 15, 2007 1:20 PM Subject: Re: Engines-List: Costly mistake I bought a project airplane a few years ago. The engine was in a hanger about 1 1/2 years with no special care, didn't even have the plugs in it. When I got it home I put Aeoshell fluid 2F in it and rotated the whole engine around a couple times, put in dehydrator plugs, then it sat for 2 years while I rebuilt the airplane. It has been a great engine, now has over 300 hrs since I bought the project. I would never suggest treating an engine that way. I would always use Aeroshell fluid2F if an engine was to be stored for over 2 month or so. If you can run the engine, I would run it, drain the oil and put in the Aeroshell fluid2F then run it again and put it away. The big worry as far as I am concerned is the cam and lifters, they will not tolerate rust. You can remove a cylinder and look inside to verify that no rust is present, no need for a tear down. My 2 pennies. Bill Becker --------------------------------- All new Yahoo! Mail - --------------------------------- Get a sneak peak at messages with a handy reading pane. ________________________________________________________________________________
From: "Dacha" <tstaley(at)centurytel.net>
Subject: Re: Costly mistake
Date: Feb 16, 2007
Ben, The engine is non turbo. Cruise between 4000-4200 rpm. All instruments are in the green, the only time it registers any excessive heat is full throttle and climbing. Not sure how the crankcase breather set up is but the belly isnt excessively dirty. Bought the plane from the builder. LeRoy ________________________________________________________________________________
Subject: Costly mistake
Date: Feb 16, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
Yes but the air (carrying the water) can't get into the case in the first place. Typically the rust appears on the cam i.e at the top of the case. The air inside the case is hot and moist when shutdown, then cools below its dewpoint and then the water condenses on the cam etc. Thus if it is full of oil there can be no air, therefore no moisture. Thats the theory at least. Frank ________________________________ From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Wayne Sweet Sent: Thursday, February 15, 2007 4:20 PM Subject: Re: Engines-List: Costly mistake I thought since oil floats on water, the condensation will get "under" the oil and bingo, rust. Wayne ----- Original Message ----- From: Hinde, Frank George (Corvallis) To: engines-list(at)matronics.com Sent: Thursday, February 15, 2007 2:02 PM Subject: RE: Engines-List: Costly mistake ________________________________ From: Sent: Thursday, February 15, 2007 1:48 PM To: 'engines-list(at)matronics.com' Subject: RE: Engines-List: Costly mistake You know one of the best preserving ideas I ever heard was to buy some cheap oil for your car and completly fill the crankcase...I.e drive out all the oil. When you get it half full turn it over slowly a couple of times, then finish filling it up. The fill up the cylinders as well if you have some scrap plugs , of course you will need to remove the rocker arms to keep the valves closed but that can't be too difficult. . No way it can rust now and you can use the oil in your car afterwards... Frank ________________________________ From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of William Becker Sent: Thursday, February 15, 2007 1:20 PM To: engines-list(at)matronics.com Subject: Re: Engines-List: Costly mistake I bought a project airplane a few years ago. The engine was in a hanger about 1 1/2 years with no special care, didn't even have the plugs in it. When I got it home I put Aeoshell fluid 2F in it and rotated the whole engine around a couple times, put in dehydrator plugs, then it sat for 2 years while I rebuilt the airplane. It has been a great engine, now has over 300 hrs since I bought the project. I would never suggest treating an engine that way. I would always use Aeroshell fluid2F if an engine was to be stored for over 2 month or so. If you can run the engine, I would run it, drain the oil and put in the Aeroshell fluid2F then run it again and put it away. The big worry as far as I am concerned is the cam and lifters, they will not tolerate rust. You can remove a cylinder and look inside to verify that no rust is present, no need for a tear down. My 2 pennies. Bill Becker href="http://www.matronics.com/Navigator?Engines-List">http://www.matro n ics.com/Navigator?Engines-List href="http://forums.matronics.com">http://forums.matronics.com ________________________________________________________________________________
From: "Cowan/Cameron" <cowcam(at)pipcom.com>
Subject: Engine storage
Date: Feb 16, 2007
Someone asked about anyone not having problems with unpickled engine. Several years ago I removed an 0360 Lycoming for an airframe re-build and left it hanging in a leaky barn. Everytime I walked by it I kicked myself for how I was treating it: no oil added anywhere and no plugs in the exhaust or intake. After maybe 4 years I decided that since I was going to sell the project it would best to send the engine into a shop to check for corrosion and top it. No problems anywhere. I live in southern Ontario Can. so see a variety of weather. Peter ________________________________________________________________________________
Date: Feb 16, 2007
From: "Bob" <rfg842(at)cox.net>
Subject: Bad engine
Thought I had all the bases covered with that 0 290-D2. Although I bough t the plane from an individual, I talked to the fixed base operator, a very reputable person, who had recovered the aircraft and majored the engine. Problem was lack of use. Sat for too many years without running regularl y and even in the dry air of Arizona, rust happens. And by the way, consumption was about a quart every four hours. Had to h ave the crank turned down to its last grinding. Really should have ditched t he engine and replaced it with a 150 hp Lyc. Bob, Wichita ________________________________________________________________________________
From: "Dacha" <tstaley(at)centurytel.net>
Subject: Re: Costly mistake
Date: Feb 16, 2007
It is an EA81. What is the fix? LeRoy ________________________________________________________________________________
Subject: Costly mistake
Date: Feb 16, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
Ahh!..It could have significant blowby on the piston rings. What happens is the cylinders are bored and then the heads torqued. this flexes the bore. The solution is to have it bored with a "boring plate" bolted down first. This simulates the torque of the head bolts. Now of course this is only one possibility and it requires an engine strip to sort it out. The EA 81 is a pretty simple engine to strip and reassemble so its not the end of the world but not something you want to do more than once. My advice is to speak with the top engine guru as far as EA81's are concerned. That would be Ron Carr at Ram Performance. A number of (so called) rebuilt Soobs had valve giudes dropping out of their heads, mine included. Ron was the only guy that came up with a permanent fix. IF you end up stripping your engine I would have him install the stepped valve guides. http://www.ramengines.com/ he is exceptionally knowlegable.. And tell him Frank said Hi.... Frank Zodiac 601HDS 400 hours RV7a 75 hours. ________________________________ From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Dacha Sent: Friday, February 16, 2007 8:23 AM Subject: Re: Engines-List: Costly mistake It is an EA81. What is the fix? LeRoy ________________________________________________________________________________
From: "Butch" <kmodairy(at)centurytel.net>
Subject: Re: Engine storage
Date: Feb 16, 2007
Thanks for the good news that not every engine goes bad. If I were to pull a jug which one would give the best view of the cam and would that screw up the ring seat for that cylinder, Thanks again ----- Original Message ----- From: Cowan/Cameron To: engines-list(at)matronics.com Sent: Friday, February 16, 2007 9:04 AM Subject: Engines-List: Engine storage Someone asked about anyone not having problems with unpickled engine. Several years ago I removed an 0360 Lycoming for an airframe re-build and left it hanging in a leaky barn. Everytime I walked by it I kicked myself for how I was treating it: no oil added anywhere and no plugs in the exhaust or intake. After maybe 4 years I decided that since I was going to sell the project it would best to send the engine into a shop to check for corrosion and top it. No problems anywhere. I live in southern Ontario Can. so see a variety of weather. Peter ________________________________________________________________________________
From: "Wayne Sweet" <w_sweet(at)comcast.net>
Subject: Re: Engine storage
Date: Feb 16, 2007
I had a maintenance shop look at my engine that was sitting for two years; they said to pull #1 and #4. That would allow to see all the cam lobes. Wayne ----- Original Message ----- From: Butch To: engines-list(at)matronics.com Sent: Friday, February 16, 2007 10:11 AM Subject: Re: Engines-List: Engine storage Thanks for the good news that not every engine goes bad. If I were to pull a jug which one would give the best view of the cam and would that screw up the ring seat for that cylinder, Thanks again ----- Original Message ----- From: Cowan/Cameron To: engines-list(at)matronics.com Sent: Friday, February 16, 2007 9:04 AM Subject: Engines-List: Engine storage Someone asked about anyone not having problems with unpickled engine. Several years ago I removed an 0360 Lycoming for an airframe re-build and left it hanging in a leaky barn. Everytime I walked by it I kicked myself for how I was treating it: no oil added anywhere and no plugs in the exhaust or intake. After maybe 4 years I decided that since I was going to sell the project it would best to send the engine into a shop to check for corrosion and top it. No problems anywhere. I live in southern Ontario Can. so see a variety of weather. Peter href="http://www.matronics.com/Navigator?Engines-List">http://www.matro nics.com/Navigator?Engines-List href="http://forums.matronics.com">http://forums.matronics.com ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Costly mistake
Date: Feb 16, 2007
If all the parts are wet with oil first there is no way for any water to get under the oil. Yes there is no point in oiling an engine that has been immersed in water That is one way that you can get water under the oil. For engines that have been immersed in water the best thing you can do is disassemble the engine to a point that you can dry the engine very quickly then oil for storage. Noel -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Wayne Sweet Sent: Thursday, February 15, 2007 8:50 PM Subject: Re: Engines-List: Costly mistake I thought since oil floats on water, the condensation will get "under" the oil and bingo, rust. Wayne ----- Original Message ----- From: Hinde, Frank <mailto:frank.hinde(at)hp.com> George (Corvallis) Sent: Thursday, February 15, 2007 2:02 PM Subject: RE: Engines-List: Costly mistake _____ From: Sent: Thursday, February 15, 2007 1:48 PM Subject: RE: Engines-List: Costly mistake You know one of the best preserving ideas I ever heard was to buy some cheap oil for your car and completly fill the crankcase...I.e drive out all the oil. When you get it half full turn it over slowly a couple of times, then finish filling it up. The fill up the cylinders as well if you have some scrap plugs , of course you will need to remove the rocker arms to keep the valves closed but that can't be too difficult. . No way it can rust now and you can use the oil in your car afterwards... Frank _____ From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of William Becker Sent: Thursday, February 15, 2007 1:20 PM Subject: Re: Engines-List: Costly mistake I bought a project airplane a few years ago. The engine was in a hanger about 1 1/2 years with no special care, didn't even have the plugs in it. When I got it home I put Aeoshell fluid 2F in it and rotated the whole engine around a couple times, put in dehydrator plugs, then it sat for 2 years while I rebuilt the airplane. It has been a great engine, now has over 300 hrs since I bought the project. I would never suggest treating an engine that way. I would always use Aeroshell fluid2F if an engine was to be stored for over 2 month or so. If you can run the engine, I would run it, drain the oil and put in the Aeroshell fluid2F then run it again and put it away. The big worry as far as I am concerned is the cam and lifters, they will not tolerate rust. You can remove a cylinder and look inside to verify that no rust is present, no need for a tear down. My 2 pennies. Bill Becker href="http://www.matronics.com/Navigator?Engines-List">http://www.matro nics. com/Navigator?Engines-List href="http://forums.matronics.com">http://forums.matronics.com ________________________________________________________________________________
From: "Dacha" <tstaley(at)centurytel.net>
Subject: Re: Costly mistake
Date: Feb 16, 2007
Talked to Ram this morning and when I have it overhauled they will be the ones to do it. Sounded very professional and knowledgeable. Not cheap but what is? LeRoy Ps. thanks to everyone who responded to my request, great list like to meet the guys sometime. ________________________________________________________________________________
From: Hopperdhh(at)aol.com
Date: Feb 16, 2007
Subject: Re: Engine storage
In a message dated 2/16/2007 1:13:59 PM Eastern Standard Time, kmodairy(at)centurytel.net writes: Thanks for the good news that not every engine goes bad. If I were to pull a jug which one would give the best view of the cam and would that screw up the ring seat for that cylinder, Thanks again No, you don't have to unseat the rings. Put the piston at top center. Pull the cylinder off far enough to just clear the wrist pin. Push the pin out and leave the piston in the cylinder. This is a two man job. You will need help getting the pin out, and also to help you to not drop the rod and mar the case. Dan Hopper RV-7A ________________________________________________________________________________
Subject: Costly mistake
Date: Feb 17, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
When your engine literally eats a chunk of valve guide and your convinced it is trying to kill you, cheap is not a consideration....When it does THREE times and the supplier still gives you a bunch of baloney about how it is your fault (namely you get the bill) then you will see that a Ram engine is very good value for money indeed. Yes Ron is bar far the most knowlegable Ea 81 guy out there. Frank ________________________________ From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Dacha Sent: Friday, February 16, 2007 2:57 PM Subject: Re: Engines-List: Costly mistake Talked to Ram this morning and when I have it overhauled they will be the ones to do it. Sounded very professional and knowledgeable. Not cheap but what is? LeRoy Ps. thanks to everyone who responded to my request, great list like to meet the guys sometime. ________________________________________________________________________________
Date: Feb 16, 2007
From: Ken <klehman(at)albedo.net>
Subject: Re: Costly mistake
Pretty close to nil on my ej22 with psru and an average 4200rpm cruise. I added a half liter of 5W50 synthetic in the last 40 hours but much of that was/is a small leak. Ken n801bh(at)netzero.com wrote: > Sooo. > > Lets get back to the original question. Frank and Joe and any other > soob flyer. What is your oil consumption??????????????????????? > > ________________________________________________________________________________
From: "Southern Reflections" <purplemoon99(at)bellsouth.net>
Subject: Re: Costly mistake
Date: Feb 16, 2007
What kind of synth. are you using? and for how long ? Joe N101HD ----- Original Message ----- From: "Ken" <klehman(at)albedo.net> Sent: Friday, February 16, 2007 10:08 PM Subject: Re: Engines-List: Costly mistake > > Pretty close to nil on my ej22 with psru and an average 4200rpm cruise. > I added a half liter of 5W50 synthetic in the last 40 hours but much of > that was/is a small leak. > Ken > > n801bh(at)netzero.com wrote: > >> Sooo. >> >> Lets get back to the original question. Frank and Joe and any other >> soob flyer. What is your oil consumption??????????????????????? >> >> > > > > > > ________________________________________________________________________________
Date: Feb 17, 2007
From: Ken <klehman(at)albedo.net>
Subject: Re: Costly mistake
Hi Joe I suspect that Mobil 1 is no longer a superior product so I use the cheaper and easier to obtain Castrol Syntec and unleaded fuel. Soob does specify 50 weight oil for this engine for heavy duty applications and it works a lot harder than it ever does in a car. My oil pan temp will get up to 120 C (250 F) on hot weather climbs and the 5W50 is also comfortable for sub freezing start ups. I only have about 65 hours on the engine since new but I'm aware of others that have run similar for a few hundred hours now. Ken Southern Reflections wrote: > > > What kind of synth. are you using? and for how long ? Joe N101HD > ----- Original Message ----- From: "Ken" <klehman(at)albedo.net> > To: > Sent: Friday, February 16, 2007 10:08 PM > Subject: Re: Engines-List: Costly mistake > > >> >> Pretty close to nil on my ej22 with psru and an average 4200rpm >> cruise. I added a half liter of 5W50 synthetic in the last 40 hours >> but much of that was/is a small leak. >> Ken >> >> n801bh(at)netzero.com wrote: >> >>> Sooo. >>> >>> Lets get back to the original question. Frank and Joe and any other >>> soob flyer. What is your oil consumption??????????????????????? >>> >>> >> >> >> >> >> >> > > ________________________________________________________________________________
From: "Gene Smith" <esmith6(at)satx.rr.com>
Subject: Engine Running Rough
Date: Feb 17, 2007
Please don't all of you shoot me at once................I have a suggestion for all of you who think your "rough" engine may be caused by internal problems...Before you spend a lot of time, labor, and money, I would install new spark plugs, new spark plug wires, and check the mags if you have mags...(I know almost all of you did this first, but maybe someone out there didn't?)...Above all, have a Pro. prop shop BALANCE your PROP while it is on the aircraft. I thought I had a problem with many of the symptoms some of you mentioned, then had that rascal prop balanced, and I really have trouble believing it is the same aircraft, it is sooo smooth, why didn't I have that done many hours ago...It cut the "worry factor" by at least 60%...........Hope I didn't insult anyone........................................CHEERS!!!! Gene Smith RV-4 ________________________________________________________________________________
From: "Wayne Sweet" <w_sweet(at)comcast.net>
Subject: Re: Engine Running Rough
Date: Feb 17, 2007
I cannot agree more; this has been exactly my experience with my MustangII. Particularily aircraft standard spark plugs; seems a lead fouled plug makes a Lycoming so sick, it runs as if two cylinders went on vacation. With CDI's and auto plugs (why would anyone run mags and "those plug"), smooth is the operative word. :-))) Wayne ----- Original Message ----- From: Gene Smith To: engines-list Sent: Saturday, February 17, 2007 5:28 PM Subject: Engines-List: Engine Running Rough Please don't all of you shoot me at once................I have a suggestion for all of you who think your "rough" engine may be caused by internal problems...Before you spend a lot of time, labor, and money, I would install new spark plugs, new spark plug wires, and check the mags if you have mags...(I know almost all of you did this first, but maybe someone out there didn't?)...Above all, have a Pro. prop shop BALANCE your PROP while it is on the aircraft. I thought I had a problem with many of the symptoms some of you mentioned, then had that rascal prop balanced, and I really have trouble believing it is the same aircraft, it is sooo smooth, why didn't I have that done many hours ago...It cut the "worry factor" by at least 60%...........Hope I didn't insult anyone........................................CHEERS!!!! Gene Smith RV-4 ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Engine Running Rough
Date: Feb 18, 2007
The reasons are laid out, basically for passenger carrying aircraft. They require redundancy and separate powered ignition systems that won't go black in the event of a catastrophic electrical problem. On the other hand yes there are some great CDI ignitions that help the engines run better than they were designed to. For amateur built aircraft I doubt there is anything better. Noel -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Wayne Sweet Sent: Sunday, February 18, 2007 12:36 AM Subject: Re: Engines-List: Engine Running Rough I cannot agree more; this has been exactly my experience with my MustangII. Particularily aircraft standard spark plugs; seems a lead fouled plug makes a Lycoming so sick, it runs as if two cylinders went on vacation. With CDI's and auto plugs (why would anyone run mags and "those plug"), smooth is the operative word. :-))) Wayne ----- Original Message ----- From: Gene <mailto:esmith6(at)satx.rr.com> Smith Sent: Saturday, February 17, 2007 5:28 PM Subject: Engines-List: Engine Running Rough Please don't all of you shoot me at once................I have a suggestion for all of you who think your "rough" engine may be caused by internal problems...Before you spend a lot of time, labor, and money, I would install new spark plugs, new spark plug wires, and check the mags if you have mags...(I know almost all of you did this first, but maybe someone out there didn't?)...Above all, have a Pro. prop shop BALANCE your PROP while it is on the aircraft. I thought I had a problem with many of the symptoms some of you mentioned, then had that rascal prop balanced, and I really have trouble believing it is the same aircraft, it is sooo smooth, why didn't I have that done many hours ago...It cut the "worry factor" by at least 60%...........Hope I didn't insult anyone........................................CHEERS!!!! Gene Smith RV-4 href="http://www.matronics.com/Navigator?Engines-List">http://www.matro nics. com/Navigator?Engines-List href="http://forums.matronics.com">http://forums.matronics.com Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-virus/ Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-virus/ ________________________________________________________________________________
From: "Archie" <archie97(at)earthlink.net>
Subject: Re: Engine Running Rough
Date: Feb 18, 2007
MessageWithout bursting bubbles. or offending the beaurocratic FAA, there is nothing better currently for any internal combustion engine than electronic ignition. Just try firing a .080 gap plug with a current magneto.(just one reason) Archie Frangoudis Archie's Racing Service ----- Original Message ----- From: Noel Loveys To: engines-list(at)matronics.com Sent: Sunday, February 18, 2007 10:47 AM Subject: RE: Engines-List: Engine Running Rough The reasons are laid out, basically for passenger carrying aircraft. They require redundancy and separate powered ignition systems that won't go black in the event of a catastrophic electrical problem. On the other hand yes there are some great CDI ignitions that help the engines run better than they were designed to. For amateur built aircraft I doubt there is anything better. Noel ________________________________________________________________________________
From: "Wayne Sweet" <w_sweet(at)comcast.net>
Subject: Re: Engine Running Rough
Date: Feb 18, 2007
MessageForgot to mention, dual CDI systems, as in my case, usually have a small battery charging from the alternator, dedicated solely to one CDI. In my plane there is a switch that in the event of primary buss failure (alternator failure is one example), this battery will run the one CDI. I have lost an alternator 45 minutes outbound from my home base. After turning off all but the transponder, the main batter still had 12.4 volts after return to home base and the backup was not needed. If one cannot find an airport in an hour flight time, then the backup will extend the range beyond a reasonable time. Of course if a buss were to fail, then the backup would power the CDI, again in my case for at least two hours. Oh, one other item, mag checks demonstrate that only one CDI is really needed, since no RPM drop is experienced when one CDI is turned off. Another checklist item; warn any right-seat pilot that no "mag drop" does not mean trouble; it means things are working fine. Wayne ----- Original Message ----- From: Archie To: engines-list(at)matronics.com Sent: Sunday, February 18, 2007 6:34 PM Subject: Re: Engines-List: Engine Running Rough Without bursting bubbles. or offending the beaurocratic FAA, there is nothing better currently for any internal combustion engine than electronic ignition. Just try firing a .080 gap plug with a current magneto.(just one reason) Archie Frangoudis Archie's Racing Service ----- Original Message ----- From: Noel Loveys To: engines-list(at)matronics.com Sent: Sunday, February 18, 2007 10:47 AM Subject: RE: Engines-List: Engine Running Rough The reasons are laid out, basically for passenger carrying aircraft. They require redundancy and separate powered ignition systems that won't go black in the event of a catastrophic electrical problem. On the other hand yes there are some great CDI ignitions that help the engines run better than they were designed to. For amateur built aircraft I doubt there is anything better. Noel ________________________________________________________________________________
Date: Feb 18, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Engine Running Rough
Depends on your definition of better. There isn't an electronic ignition made that will fire without a power source. Lose your electrics and the engine WILL quit. OK in a car, not okay in a plane. A magneto provides plenty of voltage to fire the proper gaps for aircraft plugs at all engine speeds above idle. Bureaucracy has nothing to do with it. Reliability is the prime issue with aircraft, and there simply isn't an ignition made that is more reliable than a pair of magnetos when you consider electrical failure a reasonable possibility. On 2/18/07, Archie wrote: > > > Without bursting bubbles. or offending the beaurocratic FAA, > there is nothing better currently for any internal combustion engine > than electronic ignition. > Just try firing a .080 gap plug with a current magneto.(just one reason) > Archie Frangoudis > Archie's Racing Service > > ----- Original Message ----- > From: Noel Loveys > To: engines-list(at)matronics.com > Sent: Sunday, February 18, 2007 10:47 AM > Subject: RE: Engines-List: Engine Running Rough > > > The reasons are laid out, basically for passenger carrying aircraft. They > require redundancy and separate powered ignition systems that won't go black > in the event of a catastrophic electrical problem. On the other hand yes > there are some great CDI ignitions that help the engines run better than > they were designed to. For amateur built aircraft I doubt there is anything > better. > > > Noel > > ________________________________________________________________________________
From: "Grant Piper" <grant.piper(at)bigpond.com>
Subject: Re: Engine Running Rough
Date: Feb 19, 2007
Electronic ignition is OK,but try hand-swinging when the battery is flat or the starter is broken! Also, if you get no 'mag drop' when running an EI setup, then what is the benefit of dual EI? Why not just keep one mag and have one EI, then there is no need for dual busses, the extra complexity and associated weight etc. Just my simple farmer way of thinking of things.... Grant Piper RV-4 VH-PIO ----- Original Message ----- From: "Kelly McMullen" <apilot2(at)gmail.com> Sent: Monday, February 19, 2007 3:49 PM Subject: Re: Engines-List: Engine Running Rough > > Depends on your definition of better. There isn't an electronic > ignition made that will fire without a power source. Lose your > electrics and the engine WILL quit. OK in a car, not okay in a plane. > A magneto provides plenty of voltage to fire the proper gaps for > aircraft plugs at all engine speeds above idle. Bureaucracy has > nothing to do with it. Reliability is the prime issue with aircraft, > and there simply isn't an ignition made that is more reliable than a > pair of magnetos when you consider electrical failure a reasonable > possibility. > > On 2/18/07, Archie wrote: >> >> >> Without bursting bubbles. or offending the beaurocratic FAA, >> there is nothing better currently for any internal combustion engine >> than electronic ignition. >> Just try firing a .080 gap plug with a current magneto.(just one reason) >> Archie Frangoudis >> Archie's Racing Service >> >> ----- Original Message ----- >> From: Noel Loveys >> To: engines-list(at)matronics.com >> Sent: Sunday, February 18, 2007 10:47 AM >> Subject: RE: Engines-List: Engine Running Rough >> >> >> The reasons are laid out, basically for passenger carrying aircraft. >> They >> require redundancy and separate powered ignition systems that won't go >> black >> in the event of a catastrophic electrical problem. On the other hand yes >> there are some great CDI ignitions that help the engines run better than >> they were designed to. For amateur built aircraft I doubt there is >> anything >> better. >> >> >> >> Noel >> >> >> >> > > > ________________________________________________________________________________
From: "Archie" <archie97(at)earthlink.net>
Subject: Re: Engine Running Rough
Date: Feb 19, 2007
With all due respect to your commentary, sir, I knew some replies would come from traditionalists, and I concur with your statements.. I will not deal with the semantics associated with such, but suffice it to simply say read my original message carefully. If people did not forward think in automotive, we would all still be driving model "T"'s. End. Archie Frangoudis Archie's Racing Service ----- Original Message ----- From: "Kelly McMullen" <apilot2(at)gmail.com> Sent: Sunday, February 18, 2007 11:49 PM Subject: Re: Engines-List: Engine Running Rough > > Depends on your definition of better. There isn't an electronic > ignition made that will fire without a power source. Lose your > electrics and the engine WILL quit. OK in a car, not okay in a plane. > A magneto provides plenty of voltage to fire the proper gaps for > aircraft plugs at all engine speeds above idle. Bureaucracy has > nothing to do with it. Reliability is the prime issue with aircraft, > and there simply isn't an ignition made that is more reliable than a > pair of magnetos when you consider electrical failure a reasonable > possibility. > > On 2/18/07, Archie wrote: >> >> >> Without bursting bubbles. or offending the beaurocratic FAA, >> there is nothing better currently for any internal combustion engine >> than electronic ignition. >> Just try firing a .080 gap plug with a current magneto.(just one reason) >> Archie Frangoudis >> Archie's Racing Service >> >> ----- Original Message ----- >> From: Noel Loveys >> To: engines-list(at)matronics.com >> Sent: Sunday, February 18, 2007 10:47 AM >> Subject: RE: Engines-List: Engine Running Rough >> >> >> The reasons are laid out, basically for passenger carrying aircraft. >> They >> require redundancy and separate powered ignition systems that won't go >> black >> in the event of a catastrophic electrical problem. On the other hand yes >> there are some great CDI ignitions that help the engines run better than >> they were designed to. For amateur built aircraft I doubt there is >> anything >> better. >> >> >> >> Noel >> >> >> >> > > > ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Engine Running Rough
Date: Feb 19, 2007
The answer from the FAA I'll bet would be something like try firing a .018 plug with a CDI that has no power supply. The best answer is of course one magneto and one CDI. That would give you a limp home mode in case of a problem with the CDI. BTW has anyone ever heard of a problem with a CDI while in use??? I haven't. Noel -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Archie Sent: Sunday, February 18, 2007 11:05 PM Subject: Re: Engines-List: Engine Running Rough Without bursting bubbles. or offending the beaurocratic FAA, there is nothing better currently for any internal combustion engine than electronic ignition. Just try firing a .080 gap plug with a current magneto.(just one reason) Archie Frangoudis Archie's Racing Service ----- Original Message ----- From: Noel <mailto:noelloveys(at)yahoo.ca> Loveys Sent: Sunday, February 18, 2007 10:47 AM Subject: RE: Engines-List: Engine Running Rough The reasons are laid out, basically for passenger carrying aircraft. They require redundancy and separate powered ignition systems that won't go black in the event of a catastrophic electrical problem. On the other hand yes there are some great CDI ignitions that help the engines run better than they were designed to. For amateur built aircraft I doubt there is anything better. Noel Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-virus/ Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-virus/ ________________________________________________________________________________
From: "jrc" <jrccea(at)bellsouth.net>
Subject: Re: Engine Running Rough
Date: Feb 19, 2007
MessageNo. But, I've had total power failures on two occasions..... Was grateful for mags at the time. I also fly a non-electric cub a good bit of the time, and think that might present a problem for CDI. BTW has anyone ever heard of a problem with a CDI while in use??? I haven't. Noel ________________________________________________________________________________
Date: Feb 19, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Engine Running Rough
Yeah, right. I was using CD ignition on a car 35 years ago(and it failed within 2 years). Show me an electronic ignition that is self powered and stone reliable and I'll come over to your side. So far, the automotive technology that has proven superior for aircraft, sum total, will fit in a C-150. Porsche tried and failed. Dozens have tried the aluminum Chevy, and failed. VW, Corvair, Subaru...all niche curiosities that haven't made it to mainstream. Face it. There isn't an electronic ignition that passes the dead battery test. Until that is possible, you are just bandaiding around the problem with dual buses and other backups. On 2/19/07, Archie wrote: > > With all due respect to your commentary, sir, I knew > some replies would come from traditionalists, and I concur > with your statements.. > I will not deal with the semantics associated with such, > but suffice it to simply say read my original message carefully. > If people did not forward think in automotive, we would all > still be driving model "T"'s. > End. > Archie Frangoudis > Archie's Racing Service > > ----- Original Message ----- > From: "Kelly McMullen" <apilot2(at)gmail.com> > To: > Sent: Sunday, February 18, 2007 11:49 PM > Subject: Re: Engines-List: Engine Running Rough > > > > > > Depends on your definition of better. There isn't an electronic > > ignition made that will fire without a power source. Lose your > > electrics and the engine WILL quit. OK in a car, not okay in a plane. > > A magneto provides plenty of voltage to fire the proper gaps for > > aircraft plugs at all engine speeds above idle. Bureaucracy has > > nothing to do with it. Reliability is the prime issue with aircraft, > > and there simply isn't an ignition made that is more reliable than a > > pair of magnetos when you consider electrical failure a reasonable > > possibility. > > > > On 2/18/07, Archie wrote: > >> > >> > >> Without bursting bubbles. or offending the beaurocratic FAA, > >> there is nothing better currently for any internal combustion engine > >> than electronic ignition. > >> Just try firing a .080 gap plug with a current magneto.(just one reason) > >> Archie Frangoudis > >> Archie's Racing Service > >> > >> ----- Original Message ----- > >> From: Noel Loveys > >> To: engines-list(at)matronics.com > >> Sent: Sunday, February 18, 2007 10:47 AM > >> Subject: RE: Engines-List: Engine Running Rough > >> > >> > >> The reasons are laid out, basically for passenger carrying aircraft. > >> They > >> require redundancy and separate powered ignition systems that won't go > >> black > >> in the event of a catastrophic electrical problem. On the other hand yes > >> there are some great CDI ignitions that help the engines run better than > >> they were designed to. For amateur built aircraft I doubt there is > >> anything > >> better. > >> > >> > >> > >> Noel > >> > >> > >> > >> > > > > > > > > > > > > ________________________________________________________________________________
Date: Feb 19, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Engine Running Rough
Yes. I had one on my car years ago. It flat failed and left me stranded. Something inside the box fried. On 2/19/07, Noel Loveys wrote: > > > The answer from the FAA I'll bet would be something like try firing a .018 > plug with a CDI that has no power supply. > > The best answer is of course one magneto and one CDI. That would give you a > limp home mode in case of a problem with the CDI. BTW has anyone ever heard > of a problem with a CDI while in use??? I haven't. > > Noel > > > -----Original Message----- > From: owner-engines-list-server(at)matronics.com > [mailto:owner-engines-list-server(at)matronics.com] On Behalf > Of Archie > Sent: Sunday, February 18, 2007 11:05 PM > To: engines-list(at)matronics.com > Subject: Re: Engines-List: Engine Running Rough > > > Without bursting bubbles. or offending the beaurocratic FAA, > there is nothing better currently for any internal combustion engine > than electronic ignition. > Just try firing a .080 gap plug with a current magneto.(just one reason) > Archie Frangoudis > Archie's Racing Service > > ----- Original Message ----- > From: Noel Loveys > To: engines-list(at)matronics.com > Sent: Sunday, February 18, 2007 10:47 AM > Subject: RE: Engines-List: Engine Running Rough > > > The reasons are laid out, basically for passenger carrying aircraft. They > require redundancy and separate powered ignition systems that won't go black > in the event of a catastrophic electrical problem. On the other hand yes > there are some great CDI ignitions that help the engines run better than > they were designed to. For amateur built aircraft I doubt there is anything > better. > > > Noel > > href="http://www.matronics.com/Navigator?Engines-List">http://www.matronics.com/Navigator?Engines-List > href="http://forums.matronics.com">http://forums.matronics.com > > > Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). > http://www.pctools.com/anti-v > > ________________________________________________________________________________
From: "Wayne Sweet" <w_sweet(at)comcast.net>
Subject: Re: Engine Running Rough
Date: Feb 19, 2007
I had one mag and one CDI once and it worked OK. But that means keeping those inferior aircraft plugs clean and replacing at ~$20 each. WHY? My auto plugs cost $2.50 each and are replaced every 75 hours or so. Never gap the plugs; why bother at those prices. Also, the power is somewhat better with two CDI according to Klaus Savior of LSE. I cannot confirm that. For those that have never sat behind a Lycoming running CDI's, if you do get a chance someday, ask the owner for a ride. The smoothness of the engine will surprise you. Wayne ----- Original Message ----- From: "Grant Piper" <grant.piper(at)bigpond.com> Sent: Monday, February 19, 2007 12:13 AM Subject: Re: Engines-List: Engine Running Rough > > > Electronic ignition is OK,but try hand-swinging when the battery is flat > or the starter is broken! > > Also, if you get no 'mag drop' when running an EI setup, then what is the > benefit of dual EI? Why not just keep one mag and have one EI, then > there is no need for dual busses, the extra complexity and associated > weight etc. Just my simple farmer way of thinking of things.... > > Grant Piper > RV-4 VH-PIO > > > ----- Original Message ----- > From: "Kelly McMullen" <apilot2(at)gmail.com> > To: > Sent: Monday, February 19, 2007 3:49 PM > Subject: Re: Engines-List: Engine Running Rough > > >> >> Depends on your definition of better. There isn't an electronic >> ignition made that will fire without a power source. Lose your >> electrics and the engine WILL quit. OK in a car, not okay in a plane. >> A magneto provides plenty of voltage to fire the proper gaps for >> aircraft plugs at all engine speeds above idle. Bureaucracy has >> nothing to do with it. Reliability is the prime issue with aircraft, >> and there simply isn't an ignition made that is more reliable than a >> pair of magnetos when you consider electrical failure a reasonable >> possibility. >> >> On 2/18/07, Archie wrote: >>> >>> >>> Without bursting bubbles. or offending the beaurocratic FAA, >>> there is nothing better currently for any internal combustion engine >>> than electronic ignition. >>> Just try firing a .080 gap plug with a current magneto.(just one reason) >>> Archie Frangoudis >>> Archie's Racing Service >>> >>> ----- Original Message ----- >>> From: Noel Loveys >>> To: engines-list(at)matronics.com >>> Sent: Sunday, February 18, 2007 10:47 AM >>> Subject: RE: Engines-List: Engine Running Rough >>> >>> >>> The reasons are laid out, basically for passenger carrying aircraft. >>> They >>> require redundancy and separate powered ignition systems that won't go >>> black >>> in the event of a catastrophic electrical problem. On the other hand >>> yes >>> there are some great CDI ignitions that help the engines run better than >>> they were designed to. For amateur built aircraft I doubt there is >>> anything >>> better. >>> >>> >>> >>> Noel >>> >>> >>> >>> >> >> >> >> >> > > > ________________________________________________________________________________
From: "Wayne Sweet" <w_sweet(at)comcast.net>
Subject: Re: Engine Running Rough
Date: Feb 19, 2007
See my previous post. Wayne ----- Original Message ----- From: "Kelly McMullen" <apilot2(at)gmail.com> Sent: Sunday, February 18, 2007 8:49 PM Subject: Re: Engines-List: Engine Running Rough > > Depends on your definition of better. There isn't an electronic > ignition made that will fire without a power source. Lose your > electrics and the engine WILL quit. OK in a car, not okay in a plane. > A magneto provides plenty of voltage to fire the proper gaps for > aircraft plugs at all engine speeds above idle. Bureaucracy has > nothing to do with it. Reliability is the prime issue with aircraft, > and there simply isn't an ignition made that is more reliable than a > pair of magnetos when you consider electrical failure a reasonable > possibility. > > On 2/18/07, Archie wrote: >> >> >> Without bursting bubbles. or offending the beaurocratic FAA, >> there is nothing better currently for any internal combustion engine >> than electronic ignition. >> Just try firing a .080 gap plug with a current magneto.(just one reason) >> Archie Frangoudis >> Archie's Racing Service >> >> ----- Original Message ----- >> From: Noel Loveys >> To: engines-list(at)matronics.com >> Sent: Sunday, February 18, 2007 10:47 AM >> Subject: RE: Engines-List: Engine Running Rough >> >> >> The reasons are laid out, basically for passenger carrying aircraft. >> They >> require redundancy and separate powered ignition systems that won't go >> black >> in the event of a catastrophic electrical problem. On the other hand yes >> there are some great CDI ignitions that help the engines run better than >> they were designed to. For amateur built aircraft I doubt there is >> anything >> better. >> >> >> >> Noel >> >> >> >> > > > ________________________________________________________________________________
From: "Wayne Sweet" <w_sweet(at)comcast.net>
Subject: Re: Engine Running Rough
Date: Feb 19, 2007
You are confusing CDI's of today with 35 years ago. First, cars 35 years ago were junk compared to cars of today. All cars today have electronic ignition systems; i.e. CDI's. Also the only failures I have had with alternators in my MustangII were from wire terminal failures, partly my fault for not supporting the B-wire or the field wire close the terminal. In 6000 hours of flying "store bought" airplanes only had one failure (at night in a Cardinal) that cause a complete electrical failure. If that were to happen in my plane, I would still be flying 2 hours after the failure because of the backup battery. BTW, I had a mag go south because of points coming apart after only 24 hours in service; the maintenance facility that overhauled the mag said, "That happens sometimes". WHAT!!! REALLY!!!! Lessons learned 35 years ago no longer apply today. Wayne ----- Original Message ----- From: "Kelly McMullen" <apilot2(at)gmail.com> Sent: Monday, February 19, 2007 6:13 AM Subject: Re: Engines-List: Engine Running Rough > > Yeah, right. I was using CD ignition on a car 35 years ago(and it > failed within 2 years). Show me an electronic ignition that is self > powered and stone reliable and I'll come over to your side. So far, > the automotive technology that has proven superior for aircraft, sum > total, will fit in a C-150. Porsche tried and failed. Dozens have > tried the aluminum Chevy, and failed. VW, Corvair, Subaru...all niche > curiosities that haven't made it to mainstream. Face it. There isn't > an electronic ignition that passes the dead battery test. Until that > is possible, you are just bandaiding around the problem with dual > buses and other backups. > > On 2/19/07, Archie wrote: >> >> With all due respect to your commentary, sir, I knew >> some replies would come from traditionalists, and I concur >> with your statements.. >> I will not deal with the semantics associated with such, >> but suffice it to simply say read my original message carefully. >> If people did not forward think in automotive, we would all >> still be driving model "T"'s. >> End. >> Archie Frangoudis >> Archie's Racing Service >> >> ----- Original Message ----- >> From: "Kelly McMullen" <apilot2(at)gmail.com> >> To: >> Sent: Sunday, February 18, 2007 11:49 PM >> Subject: Re: Engines-List: Engine Running Rough >> >> >> > >> > >> > Depends on your definition of better. There isn't an electronic >> > ignition made that will fire without a power source. Lose your >> > electrics and the engine WILL quit. OK in a car, not okay in a plane. >> > A magneto provides plenty of voltage to fire the proper gaps for >> > aircraft plugs at all engine speeds above idle. Bureaucracy has >> > nothing to do with it. Reliability is the prime issue with aircraft, >> > and there simply isn't an ignition made that is more reliable than a >> > pair of magnetos when you consider electrical failure a reasonable >> > possibility. >> > >> > On 2/18/07, Archie wrote: >> >> >> >> >> >> Without bursting bubbles. or offending the beaurocratic FAA, >> >> there is nothing better currently for any internal combustion engine >> >> than electronic ignition. >> >> Just try firing a .080 gap plug with a current magneto.(just one >> >> reason) >> >> Archie Frangoudis >> >> Archie's Racing Service >> >> >> >> ----- Original Message ----- >> >> From: Noel Loveys >> >> To: engines-list(at)matronics.com >> >> Sent: Sunday, February 18, 2007 10:47 AM >> >> Subject: RE: Engines-List: Engine Running Rough >> >> >> >> >> >> The reasons are laid out, basically for passenger carrying aircraft. >> >> They >> >> require redundancy and separate powered ignition systems that won't go >> >> black >> >> in the event of a catastrophic electrical problem. On the other hand >> >> yes >> >> there are some great CDI ignitions that help the engines run better >> >> than >> >> they were designed to. For amateur built aircraft I doubt there is >> >> anything >> >> better. >> >> >> >> >> >> >> >> Noel >> >> >> >> >> >> >> >> >> > >> > >> > >> > >> > >> >> >> >> >> >> >> > > > ________________________________________________________________________________
From: Hopperdhh(at)aol.com
Date: Feb 19, 2007
Subject: Re: Engine Running Rough
You will find that very few production cars today have Capacitor Discharge Ignition systems. Most systems are still inductive discharge switched by a transistor. (Transistors come in several forms including Bipolar, FET and IGBT.) This system is much simpler and more reliable than a CDI system. CDI systems are used for competition engines, though. Dan Hopper RV-7A 15 years associated with ignition design for GM including Indy CDI systems. ________________________________________________________________________________
From: "Mike" <mlas(at)cox.net>
Subject: Engine Running Rough
Date: Feb 19, 2007
So what should I do with my Airbus 320? It needs electric to run as do all the new fadec powered jet engine systems. They hide this by providing internal generators, kind of sound a little like the magneto concept. But it's not! Mike -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Monday, February 19, 2007 7:13 AM Subject: Re: Engines-List: Engine Running Rough Yeah, right. I was using CD ignition on a car 35 years ago(and it failed within 2 years). Show me an electronic ignition that is self powered and stone reliable and I'll come over to your side. So far, the automotive technology that has proven superior for aircraft, sum total, will fit in a C-150. Porsche tried and failed. Dozens have tried the aluminum Chevy, and failed. VW, Corvair, Subaru...all niche curiosities that haven't made it to mainstream. Face it. There isn't an electronic ignition that passes the dead battery test. Until that is possible, you are just bandaiding around the problem with dual buses and other backups. On 2/19/07, Archie wrote: > > With all due respect to your commentary, sir, I knew > some replies would come from traditionalists, and I concur > with your statements.. > I will not deal with the semantics associated with such, > but suffice it to simply say read my original message carefully. > If people did not forward think in automotive, we would all > still be driving model "T"'s. > End. > Archie Frangoudis > Archie's Racing Service > > ----- Original Message ----- > From: "Kelly McMullen" <apilot2(at)gmail.com> > To: > Sent: Sunday, February 18, 2007 11:49 PM > Subject: Re: Engines-List: Engine Running Rough > > > > > > Depends on your definition of better. There isn't an electronic > > ignition made that will fire without a power source. Lose your > > electrics and the engine WILL quit. OK in a car, not okay in a plane. > > A magneto provides plenty of voltage to fire the proper gaps for > > aircraft plugs at all engine speeds above idle. Bureaucracy has > > nothing to do with it. Reliability is the prime issue with aircraft, > > and there simply isn't an ignition made that is more reliable than a > > pair of magnetos when you consider electrical failure a reasonable > > possibility. > > > > On 2/18/07, Archie wrote: > >> > >> > >> Without bursting bubbles. or offending the beaurocratic FAA, > >> there is nothing better currently for any internal combustion engine > >> than electronic ignition. > >> Just try firing a .080 gap plug with a current magneto.(just one reason) > >> Archie Frangoudis > >> Archie's Racing Service > >> > >> ----- Original Message ----- > >> From: Noel Loveys > >> To: engines-list(at)matronics.com > >> Sent: Sunday, February 18, 2007 10:47 AM > >> Subject: RE: Engines-List: Engine Running Rough > >> > >> > >> The reasons are laid out, basically for passenger carrying aircraft. > >> They > >> require redundancy and separate powered ignition systems that won't go > >> black > >> in the event of a catastrophic electrical problem. On the other hand yes > >> there are some great CDI ignitions that help the engines run better than > >> they were designed to. For amateur built aircraft I doubt there is > >> anything > >> better. > >> > >> > >> > >> Noel > >> > >> > >> > >> > > > > > > > > > > > > -- 2/8/2007 -- 2/8/2007 ________________________________________________________________________________
From: "Mike" <mlas(at)cox.net>
Subject: Engine Running Rough
Date: Feb 19, 2007
Well, that's why airplanes have TWO ignition systems.... If you fly long enough you too will have a mag. failure. I have had more than 12 mags. fail, fortunately not at the same time. Mike Lancair Legacy w/dual LSE Plasma III ignitions and dual independent buses "boy it's smooth; I know it will be smoother when they quit. Ant the fuel specifics are good too." -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Monday, February 19, 2007 7:15 AM Subject: Re: Engines-List: Engine Running Rough Yes. I had one on my car years ago. It flat failed and left me stranded. Something inside the box fried. -- 2/8/2007 ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Engine Running Rough
Date: Feb 19, 2007
That would qualify as a problem with a CDI in use for me. What would you think of having one CDI and one back up magneto? Possibly using different plugs. Noel -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of jrc Sent: Monday, February 19, 2007 10:18 AM Subject: Re: Engines-List: Engine Running Rough No. But, I've had total power failures on two occasions..... Was grateful for mags at the time. I also fly a non-electric cub a good bit of the time, and think that might present a problem for CDI. BTW has anyone ever heard of a problem with a CDI while in use??? I haven't. Noel Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-virus/ Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-virus/ ________________________________________________________________________________
Subject: Engine Running Rough
Date: Feb 19, 2007
From: "Monty Barrett Sr" <MONTY(at)bpaengines.com>
NASCAR runs some type of EI. I have noticed 2 ea. MSD units in some of the TV shots. Do you reckon there is a reason for that ? I know they are not using 2 sparkplugs per chamber. Monty Barrett -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Noel Loveys Sent: Monday, February 19, 2007 10:53 AM Subject: RE: Engines-List: Engine Running Rough That would qualify as a problem with a CDI in use for me. What would you think of having one CDI and one back up magneto? Possibly using different plugs. Noel -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of jrc Sent: Monday, February 19, 2007 10:18 AM To: engines-list(at)matronics.com Subject: Re: Engines-List: Engine Running Rough No. But, I've had total power failures on two occasions..... Was grateful for mags at the time. I also fly a non-electric cub a good bit of the time, and think that might present a problem for CDI. BTW has anyone ever heard of a problem with a CDI while in use??? I haven't. Noel href="http://www.matronics.com/Navigator?Engines-List">http://www.matro n ics.com/Navigator?Engines-List href="http://forums.matronics.com">http://forums.matronics.com Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-v <http://www.pctools.com/anti-virus/> <http://www.pctools.com/anti-virus/> <http://www.pctools.com/anti-virus/> <http://www.pctools.com/anti-virus/> <http://www.pctools.com/anti-virus/> <http://www.pctools.com/anti-virus/> <http://www.pctools.com/anti-virus/> <http://www.pctools.com/anti-virus/> <http://www.pctools.com/anti-virus/> http://www.matronics.com/Navigator?Engines-List ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Engine Running Rough
Date: Feb 19, 2007
The more I read the more I think there is a case for the single mag and a single CDI. Two different technologies, two different weaknesses but when combined they could offer more protection from an engine out. One thing is for certain in the very near future there will be a big push on to clean up GA engines. Whether you start installing at least one CDI with variable timing or junk the whole lot and switch to Diesel only the future will tell. Be prepared for big changes! Noel > -----Original Message----- > From: owner-engines-list-server(at)matronics.com > [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of > Wayne Sweet > Sent: Monday, February 19, 2007 11:43 AM > To: engines-list(at)matronics.com > Subject: Re: Engines-List: Engine Running Rough > > > > > You are confusing CDI's of today with 35 years ago. First, > cars 35 years ago > were junk compared to cars of today. All cars today have > electronic ignition > systems; i.e. CDI's. > Also the only failures I have had with alternators in my > MustangII were from > wire terminal failures, partly my fault for not supporting > the B-wire or the > field wire close the terminal. In 6000 hours of flying > "store bought" > airplanes only had one failure (at night in a Cardinal) that cause a > complete electrical failure. If that were to happen in my > plane, I would > still be flying 2 hours after the failure because of the > backup battery. > BTW, I had a mag go south because of points coming apart > after only 24 hours > in service; the maintenance facility that overhauled the mag > said, "That > happens sometimes". WHAT!!! REALLY!!!! > Lessons learned 35 years ago no longer apply today. > Wayne > > ----- Original Message ----- > From: "Kelly McMullen" <apilot2(at)gmail.com> > To: > Sent: Monday, February 19, 2007 6:13 AM > Subject: Re: Engines-List: Engine Running Rough > > > > > > > Yeah, right. I was using CD ignition on a car 35 years ago(and it > > failed within 2 years). Show me an electronic ignition that is self > > powered and stone reliable and I'll come over to your side. So far, > > the automotive technology that has proven superior for aircraft, sum > > total, will fit in a C-150. Porsche tried and failed. Dozens have > > tried the aluminum Chevy, and failed. VW, Corvair, > Subaru...all niche > > curiosities that haven't made it to mainstream. Face it. There isn't > > an electronic ignition that passes the dead battery test. Until that > > is possible, you are just bandaiding around the problem with dual > > buses and other backups. > > > > On 2/19/07, Archie wrote: > > >> > >> With all due respect to your commentary, sir, I knew > >> some replies would come from traditionalists, and I concur > >> with your statements.. > >> I will not deal with the semantics associated with such, > >> but suffice it to simply say read my original message carefully. > >> If people did not forward think in automotive, we would all > >> still be driving model "T"'s. > >> End. > >> Archie Frangoudis > >> Archie's Racing Service > >> > >> ----- Original Message ----- > >> From: "Kelly McMullen" <apilot2(at)gmail.com> > >> To: > >> Sent: Sunday, February 18, 2007 11:49 PM > >> Subject: Re: Engines-List: Engine Running Rough > >> > >> > >> > > >> > > >> > Depends on your definition of better. There isn't an electronic > >> > ignition made that will fire without a power source. Lose your > >> > electrics and the engine WILL quit. OK in a car, not > okay in a plane. > >> > A magneto provides plenty of voltage to fire the proper gaps for > >> > aircraft plugs at all engine speeds above idle. Bureaucracy has > >> > nothing to do with it. Reliability is the prime issue > with aircraft, > >> > and there simply isn't an ignition made that is more > reliable than a > >> > pair of magnetos when you consider electrical failure a > reasonable > >> > possibility. > >> > > >> > On 2/18/07, Archie wrote: > >> >> > >> >> > >> >> Without bursting bubbles. or offending the beaurocratic FAA, > >> >> there is nothing better currently for any internal > combustion engine > >> >> than electronic ignition. > >> >> Just try firing a .080 gap plug with a current > magneto.(just one > >> >> reason) > >> >> Archie Frangoudis > >> >> Archie's Racing Service > >> >> > >> >> ----- Original Message ----- > >> >> From: Noel Loveys > >> >> To: engines-list(at)matronics.com > >> >> Sent: Sunday, February 18, 2007 10:47 AM > >> >> Subject: RE: Engines-List: Engine Running Rough > >> >> > >> >> > >> >> The reasons are laid out, basically for passenger > carrying aircraft. > >> >> They > >> >> require redundancy and separate powered ignition > systems that won't go > >> >> black > >> >> in the event of a catastrophic electrical problem. On > the other hand > >> >> yes > >> >> there are some great CDI ignitions that help the > engines run better > >> >> than > >> >> they were designed to. For amateur built aircraft I > doubt there is > >> >> anything > >> >> better. > >> >> > >> >> > >> >> > >> >> Noel > >> >> > >> >> > >> >> > >> >> > >> > > >> > > >> > > >> > > >> > > >> > >> > >> > >> > >> > >> > >> > > > > > > > > > > > > > > > > > > > Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). > http://www.pctools.com/anti-virus/ Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-virus/ ________________________________________________________________________________
From: "Terry Watson" <terry(at)tcwatson.com>
Subject: Engine Running Rough
Date: Feb 19, 2007
I am surprised no one has yet mentioned E-mags in this thread. http://www.emagair.com/Intro.htm I have no experience with them but the reports of their product and service have been excellent. In essence it is an electronic ignition that is a bolt-on replacement for a mag. One model requires outside power, but the other has its own built-in electrical source. Terry -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Mike Sent: Monday, February 19, 2007 7:58 AM Subject: RE: Engines-List: Engine Running Rough Well, that's why airplanes have TWO ignition systems.... If you fly long enough you too will have a mag. failure. I have had more than 12 mags. fail, fortunately not at the same time. Mike Lancair Legacy w/dual LSE Plasma III ignitions and dual independent buses "boy it's smooth; I know it will be smoother when they quit. Ant the fuel specifics are good too." -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Monday, February 19, 2007 7:15 AM Subject: Re: Engines-List: Engine Running Rough Yes. I had one on my car years ago. It flat failed and left me stranded. Something inside the box fried. -- 2/8/2007 ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Engine Running Rough
Date: Feb 19, 2007
They also have more than one generator. More than one engine. %They can sustain flight on one engine. If they have a massive electrical failure in flight the engines won't just stop and become huge anchors. If the lights in the cockpit wouldn't tell the crew they wouldn't even know about the power loss. Noel > -----Original Message----- > From: owner-engines-list-server(at)matronics.com > [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Mike > Sent: Monday, February 19, 2007 12:20 PM > To: engines-list(at)matronics.com > Subject: RE: Engines-List: Engine Running Rough > > > > So what should I do with my Airbus 320? It needs electric to > run as do > all the new fadec powered jet engine systems. They hide this by > providing internal generators, kind of sound a little like the magneto > concept. But it's not! > > Mike > > -----Original Message----- > From: owner-engines-list-server(at)matronics.com > [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Kelly > McMullen > Sent: Monday, February 19, 2007 7:13 AM > To: engines-list(at)matronics.com > Subject: Re: Engines-List: Engine Running Rough > > > > Yeah, right. I was using CD ignition on a car 35 years ago(and it > failed within 2 years). Show me an electronic ignition that is self > powered and stone reliable and I'll come over to your side. So far, > the automotive technology that has proven superior for aircraft, sum > total, will fit in a C-150. Porsche tried and failed. Dozens have > tried the aluminum Chevy, and failed. VW, Corvair, Subaru...all niche > curiosities that haven't made it to mainstream. Face it. There isn't > an electronic ignition that passes the dead battery test. Until that > is possible, you are just bandaiding around the problem with dual > buses and other backups. > > On 2/19/07, Archie wrote: > > > > > With all due respect to your commentary, sir, I knew > > some replies would come from traditionalists, and I concur > > with your statements.. > > I will not deal with the semantics associated with such, > > but suffice it to simply say read my original message carefully. > > If people did not forward think in automotive, we would all > > still be driving model "T"'s. > > End. > > Archie Frangoudis > > Archie's Racing Service > > > > ----- Original Message ----- > > From: "Kelly McMullen" <apilot2(at)gmail.com> > > To: > > Sent: Sunday, February 18, 2007 11:49 PM > > Subject: Re: Engines-List: Engine Running Rough > > > > > > > > > > > Depends on your definition of better. There isn't an electronic > > > ignition made that will fire without a power source. Lose your > > > electrics and the engine WILL quit. OK in a car, not okay in a > plane. > > > A magneto provides plenty of voltage to fire the proper gaps for > > > aircraft plugs at all engine speeds above idle. Bureaucracy has > > > nothing to do with it. Reliability is the prime issue > with aircraft, > > > and there simply isn't an ignition made that is more > reliable than a > > > pair of magnetos when you consider electrical failure a reasonable > > > possibility. > > > > > > On 2/18/07, Archie wrote: > > >> > > >> > > >> Without bursting bubbles. or offending the beaurocratic FAA, > > >> there is nothing better currently for any internal combustion > engine > > >> than electronic ignition. > > >> Just try firing a .080 gap plug with a current magneto.(just one > reason) > > >> Archie Frangoudis > > >> Archie's Racing Service > > >> > > >> ----- Original Message ----- > > >> From: Noel Loveys > > >> To: engines-list(at)matronics.com > > >> Sent: Sunday, February 18, 2007 10:47 AM > > >> Subject: RE: Engines-List: Engine Running Rough > > >> > > >> > > >> The reasons are laid out, basically for passenger carrying > aircraft. > > >> They > > >> require redundancy and separate powered ignition systems > that won't > go > > >> black > > >> in the event of a catastrophic electrical problem. On the other > hand yes > > >> there are some great CDI ignitions that help the engines > run better > than > > >> they were designed to. For amateur built aircraft I > doubt there is > > >> anything > > >> better. > > >> > > >> > > >> > > >> Noel > > >> > > >> > > >> > > >> > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > > -- > 2/8/2007 > > > -- > 2/8/2007 > > > > > > > > > Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). > http://www.pctools.com/anti-virus/ > Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-virus/ ________________________________________________________________________________
Date: Feb 19, 2007
From: Charlie England <ceengland(at)bellsouth.net>
Subject: Re: Engine Running Rough
Kelly McMullen wrote: > > Yeah, right. I was using CD ignition on a car 35 years ago(and it > failed within 2 years). Show me an electronic ignition that is self > powered and stone reliable and I'll come over to your side. So far, > the automotive technology that has proven superior for aircraft, sum > total, will fit in a C-150. Porsche tried and failed. Dozens have > tried the aluminum Chevy, and failed. VW, Corvair, Subaru...all niche > curiosities that haven't made it to mainstream. Face it. There isn't > an electronic ignition that passes the dead battery test. Until that > is possible, you are just bandaiding around the problem with dual > buses and other backups. For those who don't know yet and are trying to learn: Mags fail. Mags fail with some frequency. There's typically only one carb or injection controller, but there are almost always 2 mags. It ain't just about better combustion. If standalone ignition floats your boat, google 'p-mag' & 'e-mag' to come close to the 'ideal'. Charlie ________________________________________________________________________________
Date: Feb 19, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Engine Running Rough
No, no confusion. Also had later factory electronic ignition leave me stranded at -40. They have several points of failure. Can't tell you how many engine management CPUs get changed out regularly. Alternators are no more reliable than they ever were. All fine for cars. Not so fine for aviation. A mag failure shortly after overhaul indicates a shop that is incompetent. I have yet to have a mag actually fail in 35 years of flying. Had P-lead short a mag to ground, but no mag failure. You are welcome to go complex electronics. Your choice. That is what experimental is all about. On 2/19/07, Wayne Sweet wrote: > > You are confusing CDI's of today with 35 years ago. First, cars 35 years ago > were junk compared to cars of today. All cars today have electronic ignition > systems; i.e. CDI's. > Also the only failures I have had with alternators in my MustangII were from > wire terminal failures, partly my fault for not supporting the B-wire or the > field wire close the terminal. In 6000 hours of flying "store bought" > airplanes only had one failure (at night in a Cardinal) that cause a > complete electrical failure. If that were to happen in my plane, I would > still be flying 2 hours after the failure because of the backup battery. > BTW, I had a mag go south because of points coming apart after only 24 hours > in service; the maintenance facility that overhauled the mag said, "That > happens sometimes". WHAT!!! REALLY!!!! > Lessons learned 35 years ago no longer apply today. > Wayne > > ----- Original Message ----- > From: "Kelly McMullen" <apilot2(at)gmail.com> > To: > Sent: Monday, February 19, 2007 6:13 AM > Subject: Re: Engines-List: Engine Running Rough > > > > > > Yeah, right. I was using CD ignition on a car 35 years ago(and it > > failed within 2 years). Show me an electronic ignition that is self > > powered and stone reliable and I'll come over to your side. So far, > > the automotive technology that has proven superior for aircraft, sum > > total, will fit in a C-150. Porsche tried and failed. Dozens have > > tried the aluminum Chevy, and failed. VW, Corvair, Subaru...all niche > > curiosities that haven't made it to mainstream. Face it. There isn't > > an electronic ignition that passes the dead battery test. Until that > > is possible, you are just bandaiding around the problem with dual > > buses and other backups. > > > > On 2/19/07, Archie wrote: > >> > >> With all due respect to your commentary, sir, I knew > >> some replies would come from traditionalists, and I concur > >> with your statements.. > >> I will not deal with the semantics associated with such, > >> but suffice it to simply say read my original message carefully. > >> If people did not forward think in automotive, we would all > >> still be driving model "T"'s. > >> End. > >> Archie Frangoudis > >> Archie's Racing Service > >> > >> ----- Original Message ----- > >> From: "Kelly McMullen" <apilot2(at)gmail.com> > >> To: > >> Sent: Sunday, February 18, 2007 11:49 PM > >> Subject: Re: Engines-List: Engine Running Rough > >> > >> > >> > > >> > > >> > Depends on your definition of better. There isn't an electronic > >> > ignition made that will fire without a power source. Lose your > >> > electrics and the engine WILL quit. OK in a car, not okay in a plane. > >> > A magneto provides plenty of voltage to fire the proper gaps for > >> > aircraft plugs at all engine speeds above idle. Bureaucracy has > >> > nothing to do with it. Reliability is the prime issue with aircraft, > >> > and there simply isn't an ignition made that is more reliable than a > >> > pair of magnetos when you consider electrical failure a reasonable > >> > possibility. > >> > > >> > On 2/18/07, Archie wrote: > >> >> > >> >> > >> >> Without bursting bubbles. or offending the beaurocratic FAA, > >> >> there is nothing better currently for any internal combustion engine > >> >> than electronic ignition. > >> >> Just try firing a .080 gap plug with a current magneto.(just one > >> >> reason) > >> >> Archie Frangoudis > >> >> Archie's Racing Service > >> >> > >> >> ----- Original Message ----- > >> >> From: Noel Loveys > >> >> To: engines-list(at)matronics.com > >> >> Sent: Sunday, February 18, 2007 10:47 AM > >> >> Subject: RE: Engines-List: Engine Running Rough > >> >> > >> >> > >> >> The reasons are laid out, basically for passenger carrying aircraft. > >> >> They > >> >> require redundancy and separate powered ignition systems that won't go > >> >> black > >> >> in the event of a catastrophic electrical problem. On the other hand > >> >> yes > >> >> there are some great CDI ignitions that help the engines run better > >> >> than > >> >> they were designed to. For amateur built aircraft I doubt there is > >> >> anything > >> >> better. > >> >> > >> >> > >> >> > >> >> Noel > >> >> > >> >> > >> >> > >> >> > >> > > >> > > >> > > >> > > >> > > >> > >> > >> > >> > >> > >> > >> > > > > > > > > > > > > ________________________________________________________________________________
From: "Archie" <archie97(at)earthlink.net>
Subject: Re: Engine Running Rough
Date: Feb 19, 2007
MessageThere is an interior switch that will run one or the other. (just in case) ----- Original Message ----- From: Monty Barrett Sr To: engines-list(at)matronics.com Sent: Monday, February 19, 2007 12:03 PM Subject: RE: Engines-List: Engine Running Rough NASCAR runs some type of EI. I have noticed 2 ea. MSD units in some of the TV shots. Do you reckon there is a reason for that ? I know they are not using 2 sparkplugs per chamber. Monty Barrett -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Noel Loveys Sent: Monday, February 19, 2007 10:53 AM To: engines-list(at)matronics.com Subject: RE: Engines-List: Engine Running Rough That would qualify as a problem with a CDI in use for me. What would you think of having one CDI and one back up magneto? Possibly using different plugs. Noel -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of jrc Sent: Monday, February 19, 2007 10:18 AM To: engines-list(at)matronics.com Subject: Re: Engines-List: Engine Running Rough No. But, I've had total power failures on two occasions..... Was grateful for mags at the time. I also fly a non-electric cub a good bit of the time, and think that might present a problem for CDI. BTW has anyone ever heard of a problem with a CDI while in use??? I haven't. Noel href="http://www.matronics.com/Navigator?Engines-List">http://www.matro nics.com/Navigator?Engines-Listhref="http://forums.matronics.com">http: //forums.matronics.com Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-v http://www.matronics.com/Navigator?Engines-Listhttp://forums.matronics.co m ________________________________________________________________________________
From: Speedy11(at)aol.com
Date: Feb 19, 2007
Subject: Re: Engine Running Rough
Kelly, No wholly true. P Mags (emagair.com) is an electronic ignition that has its own internal generator such that should the electrics fail, it can continue running at speeds above idle (about 700 rpm) therefore performing essentially like a mag. When power is available, it enjoys the advantages of electronic ignition. Stan Sutterfield There isn't an electronic ignition made that will fire without a power source. Lose your electrics and the engine WILL quit. OK in a car, not okay in a plane. A magneto provides plenty of voltage to fire the proper gaps for aircraft plugs at all engine speeds above idle. ________________________________________________________________________________
Date: Feb 19, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Engine Running Rough
Yes, I was aware of PMag and it probably is as good an alternative as you can get for a 4 cyl engine. However, it isn't available for a 6 cylinder yet, and: "Even the P-MAG model needs some source of outside power at start-up. If you are prop starting because the battery is "low", there is plenty of power for the ignition. If you're battery is "almost" dead (you only get a faint glow from the cabin light) you probably have enough power for the ignition. However if you're battery is removed or is absolutely/totally dead, you cannot prop start with the electronic ignition and "no" outside power. " On 2/19/07, Speedy11(at)aol.com wrote: > > > Kelly, > No wholly true. > P Mags (emagair.com) is an electronic ignition that has its own internal > generator such that should the electrics fail, it can continue running at > speeds above idle (about 700 rpm) therefore performing essentially like a > mag. When power is available, it enjoys the advantages of electronic > ignition. > Stan Sutterfield > > There isn't an electronic > ignition made that will fire without a power source. Lose your > electrics and the engine WILL quit. OK in a car, not okay in a plane. > A magneto provides plenty of voltage to fire the proper gaps for > aircraft plugs at all engine speeds above idle. > > ________________________________________________________________________________
From: "Doug Dodson" <douglas.dodson(at)pobox.com>
Subject: Engine Running Rough
Date: Feb 20, 2007
There are many more benefits to a dual electrical system than just the ignition system. If a required vacuum system is replaced by a second battery and/or alternator, then failure of a primary (electric) gyro is reduced dramatically. The additional cost, weight and complexity is negligible (and for some designs, even negative). Magnetos are far more failure prone than CDI ignition systems. One mag, one EI means you will be spending time and money on the mag for to keep the redundancy. Parts commonality is a benefit of two identical systems. Douglas L. Dodson, Jr. Glasair II-S FT Flight Test Engineer, CFI-A,G -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com]On Behalf Of Grant Piper Sent: Monday, February 19, 2007 12:13 AM Subject: Re: Engines-List: Engine Running Rough Electronic ignition is OK,but try hand-swinging when the battery is flat or the starter is broken! Also, if you get no 'mag drop' when running an EI setup, then what is the benefit of dual EI? Why not just keep one mag and have one EI, then there is no need for dual busses, the extra complexity and associated weight etc. Just my simple farmer way of thinking of things.... Grant Piper RV-4 VH-PIO ----- Original Message ----- From: "Kelly McMullen" <apilot2(at)gmail.com> Sent: Monday, February 19, 2007 3:49 PM Subject: Re: Engines-List: Engine Running Rough > > Depends on your definition of better. There isn't an electronic > ignition made that will fire without a power source. Lose your > electrics and the engine WILL quit. OK in a car, not okay in a plane. > A magneto provides plenty of voltage to fire the proper gaps for > aircraft plugs at all engine speeds above idle. Bureaucracy has > nothing to do with it. Reliability is the prime issue with aircraft, > and there simply isn't an ignition made that is more reliable than a > pair of magnetos when you consider electrical failure a reasonable > possibility. > > On 2/18/07, Archie wrote: >> >> >> Without bursting bubbles. or offending the beaurocratic FAA, >> there is nothing better currently for any internal combustion engine >> than electronic ignition. >> Just try firing a .080 gap plug with a current magneto.(just one reason) >> Archie Frangoudis >> Archie's Racing Service >> >> ----- Original Message ----- >> From: Noel Loveys >> To: engines-list(at)matronics.com >> Sent: Sunday, February 18, 2007 10:47 AM >> Subject: RE: Engines-List: Engine Running Rough >> >> >> The reasons are laid out, basically for passenger carrying aircraft. >> They >> require redundancy and separate powered ignition systems that won't go >> black >> in the event of a catastrophic electrical problem. On the other hand yes >> there are some great CDI ignitions that help the engines run better than >> they were designed to. For amateur built aircraft I doubt there is >> anything >> better. >> >> >> >> Noel >> >> >> >> > > ________________________________________________________________________________
Date: Feb 20, 2007
From: "Bob" <rfg842(at)cox.net>
Subject: Auto plugs
Didn't have time to read all of the last comments but how does an engine act with firing auto plugs with a magneto? At the cost of aviation shielded plugs, changing to auto plugs is an incentive. Any need to change plug gaps? Bob, Wichita ________________________________________________________________________________
From: "n801bh(at)netzero.com" <n801bh(at)netzero.com>
Date: Feb 20, 2007
Subject: Re: Auto plugs
NOPE !!!!!! Ben Haas N801BH www.haaspowerair.com -- "Bob" wrote: Didn't have time to read all of the last comments but how does an engine act with firing auto plugs with a magneto? At the cost of aviation shie lded plugs, changing to auto plugs is an incentive. Any need to change ======================== ======================== ======================== ======================== ======= NOPE !!!!!!


Ben Haas
N801BH
www.haaspowerair .com

-- "Bob" <rfg842(at)cox.net> wrote:
Didn't have time to read all of the last comments but how does an e ngine act with firing auto plugs with a magneto?
 
At the cost of aviation shielded plugs, changing to auto plugs is a n incentive.  Any need to change plug gaps?
 
Bob, Wichita

      Add FUN to your email - CLICK HERE!http://www2.incre dimail.com/contents/stamps/imstp_heads_en.gif" align=baseline border= 0>

      
      ========================
      ===========
      t">http://www.matronics.com/Navigator?Engines-List>
      ========================
      ===========
      tronics.com
      ========================
      ===========
      
      

      
      
      
________________________________________________________________________________
Date: Feb 20, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Engine Running Rough
An interesting opinion, not based in fact. A dual electrical system requires two alternators(heavier than a vacuum pump and one alternator), two batteries(Significant extra wt), two totally separate buses. If you interconnect them, you leave the possibility of one failure taking out both systems. If you don't interconnect you have to be able to live with what is on either bus by itself, which means you will need some additional duplication. That is not simpler, nor less complex. I have yet to see a failure-proof electrical system. Better to have enough to keep flying when(not if) the electrics fail. I have yet to see a CDI system that is more reliable than properly maintained magnetos, in 35 years of flying and maintaining aircraft and autos. The P-Mag/Emag(and others) may change that, eventually. They have been talking certification for several years. Prism from GAMI holds a lot of promise when it gets certified. The main mag failures you see are when folks try to skimp and run magnetos 1000+ hours without service. They should be opened and inspected every 500 hours. Sometimes folks have to relearn hard lessons all over again. You are free to do that with experimental aircraft. KM A&P/IA CP ASMEL-I On 2/20/07, Doug Dodson wrote: > > There are many more benefits to a dual electrical system than just the > ignition system. If a required vacuum system is replaced by a second > battery and/or alternator, then failure of a primary (electric) gyro is > reduced dramatically. The additional cost, weight and complexity is > negligible (and for some designs, even negative). > > Magnetos are far more failure prone than CDI ignition systems. One mag, one > EI means you will be spending time and money on the mag for to keep the > redundancy. Parts commonality is a benefit of two identical systems. > > Douglas L. Dodson, Jr. > Glasair II-S FT > Flight Test Engineer, CFI-A,G > ________________________________________________________________________________
From: "Mike" <mlas(at)cox.net>
Subject: Engine Running Rough
Date: Feb 20, 2007
I agree. Mike Larkin -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Doug Dodson Sent: Tuesday, February 20, 2007 6:45 AM Subject: RE: Engines-List: Engine Running Rough There are many more benefits to a dual electrical system than just the ignition system. If a required vacuum system is replaced by a second battery and/or alternator, then failure of a primary (electric) gyro is reduced dramatically. The additional cost, weight and complexity is negligible (and for some designs, even negative). Magnetos are far more failure prone than CDI ignition systems. One mag, one EI means you will be spending time and money on the mag for to keep the redundancy. Parts commonality is a benefit of two identical systems. Douglas L. Dodson, Jr. Glasair II-S FT Flight Test Engineer, CFI-A,G -- 2/8/2007 ________________________________________________________________________________
From: "Wayne Sweet" <w_sweet(at)comcast.net>
Subject: Re: Engine Running Rough
Date: Feb 20, 2007
I agree. My plane also does not have the stupid vacuum systems either. Dynon D10A EFIS WITH internal battery backup. Is it not time to move past "the Past" and come into the 21st Century. I had the chance to fly in a Columbia 350 with the older Avidyne glass panel; very nice. BUT IT STILL HAS A VACUUM SYSTEM! GEZZZZZ! Wayne ----- Original Message ----- From: "Doug Dodson" <douglas.dodson(at)pobox.com> Sent: Tuesday, February 20, 2007 5:45 AM Subject: RE: Engines-List: Engine Running Rough > > > There are many more benefits to a dual electrical system than just the > ignition system. If a required vacuum system is replaced by a second > battery and/or alternator, then failure of a primary (electric) gyro is > reduced dramatically. The additional cost, weight and complexity is > negligible (and for some designs, even negative). > > Magnetos are far more failure prone than CDI ignition systems. One mag, > one > EI means you will be spending time and money on the mag for to keep the > redundancy. Parts commonality is a benefit of two identical systems. > > Douglas L. Dodson, Jr. > Glasair II-S FT > Flight Test Engineer, CFI-A,G > > -----Original Message----- > From: owner-engines-list-server(at)matronics.com > [mailto:owner-engines-list-server(at)matronics.com]On Behalf Of Grant Piper > Sent: Monday, February 19, 2007 12:13 AM > To: engines-list(at)matronics.com > Subject: Re: Engines-List: Engine Running Rough > > > > > Electronic ignition is OK,but try hand-swinging when the battery is flat > or > the starter is broken! > > Also, if you get no 'mag drop' when running an EI setup, then what is the > benefit of dual EI? Why not just keep one mag and have one EI, then > there > is no need for dual busses, the extra complexity and associated weight > etc. > Just my simple farmer way of thinking of things.... > > Grant Piper > RV-4 VH-PIO > > > ----- Original Message ----- > From: "Kelly McMullen" <apilot2(at)gmail.com> > To: > Sent: Monday, February 19, 2007 3:49 PM > Subject: Re: Engines-List: Engine Running Rough > > >> >> Depends on your definition of better. There isn't an electronic >> ignition made that will fire without a power source. Lose your >> electrics and the engine WILL quit. OK in a car, not okay in a plane. >> A magneto provides plenty of voltage to fire the proper gaps for >> aircraft plugs at all engine speeds above idle. Bureaucracy has >> nothing to do with it. Reliability is the prime issue with aircraft, >> and there simply isn't an ignition made that is more reliable than a >> pair of magnetos when you consider electrical failure a reasonable >> possibility. >> >> On 2/18/07, Archie wrote: >>> >>> >>> Without bursting bubbles. or offending the beaurocratic FAA, >>> there is nothing better currently for any internal combustion engine >>> than electronic ignition. >>> Just try firing a .080 gap plug with a current magneto.(just one reason) >>> Archie Frangoudis >>> Archie's Racing Service >>> >>> ----- Original Message ----- >>> From: Noel Loveys >>> To: engines-list(at)matronics.com >>> Sent: Sunday, February 18, 2007 10:47 AM >>> Subject: RE: Engines-List: Engine Running Rough >>> >>> >>> The reasons are laid out, basically for passenger carrying aircraft. >>> They >>> require redundancy and separate powered ignition systems that won't go >>> black >>> in the event of a catastrophic electrical problem. On the other hand >>> yes >>> there are some great CDI ignitions that help the engines run better than >>> they were designed to. For amateur built aircraft I doubt there is >>> anything >>> better. >>> >>> >>> >>> Noel >>> >>> >>> >>> >> >> >> >> >> > > > ________________________________________________________________________________
From: "Wayne Sweet" <w_sweet(at)comcast.net>
Subject: Re: Auto plugs
Date: Feb 20, 2007
First problem, the ignition harness will not work with auto plugs. To make things simple, just get LSE's CDI dual system, Dynon EFIS D10A or whatever EFIS you like and be done with "the Past". Wayne ----- Original Message ----- From: Bob To: engines-list(at)matronics.com Sent: Tuesday, February 20, 2007 5:44 AM Subject: Engines-List: Auto plugs Didn't have time to read all of the last comments but how does an engine act with firing auto plugs with a magneto? At the cost of aviation shielded plugs, changing to auto plugs is an incentive. Any need to change plug gaps? Bob, Wichita ________________________________________________________________________________
From: "Peter C" <peterc(at)pipcom.com>
Subject: Battery choice
Date: Feb 20, 2007
In the experimental environment for the average low tech, low power (but also low temp winters) requirements (Rotax 912S 100hp), is the extra expense of the RG batteries worth it? I once put an Odyssey 680 in a Mazda 13b aircraft replacing a cheap utility battery and wasn't all that impressed with cranking capacity and shelf life. When a friend wanted to order a larger RG for his 210 the local flying club maintenance guy said they tried them in their school aircraft and also didn't stay with them. What is the data on these batteries? Is "Immobilized electrolyte" the same as Recombinant gas? Thanks Peter ________________________________________________________________________________
Date: Feb 20, 2007
From: Daniel Tappan <dancfi(at)yahoo.com>
Subject: Re: Auto plugs
: NOPE !!!!!! Hey Bob..NOPE AGAIN !. ..the WIRES ends are different and each engine is designed or reguires a specific aircraft plug.The "reach" or distance the plug sticks down into the cylender is different on some plugs. Also There is a "Heat range"for different plugs as I remember (Can anyone out there add to this..I forgot what I knew!).. Having said all that .some of the older aircraft, Tcraft ect. used iesman mags and DID use auto spark plugs.They worked for low , slow older aircraft but were not considered a great mag. --------------------------------- TV dinner still cooling? Check out "Tonight's Picks" on Yahoo! TV. ________________________________________________________________________________
From: "jrc" <jrccea(at)bellsouth.net>
Subject: Re: Engine Running Rough
Date: Feb 20, 2007
Guys, I fly a non-electric J-3. My goal is to keep it as light as possible. In what way would a dual electrical system benefit me? :-) ----- Original Message ----- > > There are many more benefits to a dual electrical system than just the > ignition system. ________________________________________________________________________________
From: "Archie" <archie97(at)earthlink.net>
Subject: Re: Auto plugs
Date: Feb 20, 2007
----- Original Message ----- From: Bob To: engines-list(at)matronics.com Sent: Tuesday, February 20, 2007 8:44 AM Subject: Engines-List: Auto plugs Didn't have time to read all of the last comments but how does an engine act with firing auto plugs with a magneto? We have done it for customers. They like it $$$$$. At the cost of aviation shielded plugs, changing to auto plugs is an incentive. Any need to change plug gaps? As magnetos will not fire a large gap, we have only set them at .020. We have set electronics to .070/.080 to maximize spark. (and they do not need a wind-up spring. aka: impulse coupling) Bob, Wichita ________________________________________________________________________________
From: "Mike" <mlas(at)cox.net>
Subject: Engine Running Rough
Date: Feb 20, 2007
Kelly, If you use have a dual electrical system it requires two alternators yes. A small 20 amp B&C alternator is very close to the weight of a vacuum pump, drive, regulator, and required plumbing. And the B&C alternator in my very small 13,000+ hours of flying and my 30 year of aircraft maintenance shows the it should be much more reliable. If you need a 30 amp hour or more battery like a G-35 for starting then two smaller Odyssey batteries will give you the same start power for less weight. And if you are as paranoid as you sound then an old fashion gang switch for the system inter connect with a safety strap for you will keep the system disconnected in flight. As for your following statements about reliability, almost everything works without failure if properly maintained. The electrical system is in my experience the most under maintained system in an airplane. How many Cessna's have you looked at where ALL of the switches are 30 plus years old. The simple fact is that most people don't do anything to an electrical system until something fails. As far as fail proof, I fly airplanes of all types; little, middle, and big over 800 hours a year and so far I have not experienced a total electrical failure to a dark plane. As for the P-mag, I recovered an RV-7 from a highway two weekends ago when Both P-mags failed. Guess what, the electrical system worked perfectly...... Mike Larkin ATP MEL, Com SEL, Many Types Rat., A&P, & IE Lancair Legacy Build and Flown by Me TS-11 Iskra Restored and Flown by Me Kitfox IV re-engined and Flown by Me A320/319 Flown by Me.... Ps- I only get this way with very very closed minded people..... -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Tuesday, February 20, 2007 7:47 AM Subject: Re: Engines-List: Engine Running Rough An interesting opinion, not based in fact. A dual electrical system requires two alternators(heavier than a vacuum pump and one alternator), two batteries(Significant extra wt), two totally separate buses. If you interconnect them, you leave the possibility of one failure taking out both systems. If you don't interconnect you have to be able to live with what is on either bus by itself, which means you will need some additional duplication. That is not simpler, nor less complex. I have yet to see a failure-proof electrical system. Better to have enough to keep flying when(not if) the electrics fail. I have yet to see a CDI system that is more reliable than properly maintained magnetos, in 35 years of flying and maintaining aircraft and autos. The P-Mag/Emag(and others) may change that, eventually. They have been talking certification for several years. Prism from GAMI holds a lot of promise when it gets certified. The main mag failures you see are when folks try to skimp and run magnetos 1000+ hours without service. They should be opened and inspected every 500 hours. Sometimes folks have to relearn hard lessons all over again. You are free to do that with experimental aircraft. KM A&P/IA CP ASMEL-I -- 2/8/2007 ________________________________________________________________________________
Subject: Engine Running Rough
Date: Feb 20, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
Hello Mike, If this is the same incident I don't think the Pmags actually both failed, although the effect was similar. What I think probably happened was the timing on one of the P mags went way advanced. In this scenario the second Pmag is just along for the ride, i.e it sparks but the charge has already been lit at that point and hence doesn't do anything. This is still the subject of investigation as we speak...I certainly hope they find it 'cus I run Pmags myself. I think kelly's point was that the traditional magnetoes are more reliable than Pmags. Frank -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Mike Sent: Tuesday, February 20, 2007 9:51 AM Subject: RE: Engines-List: Engine Running Rough Kelly, If you use have a dual electrical system it requires two alternators yes. A small 20 amp B&C alternator is very close to the weight of a vacuum pump, drive, regulator, and required plumbing. And the B&C alternator in my very small 13,000+ hours of flying and my 30 year of aircraft maintenance shows the it should be much more reliable. If you need a 30 amp hour or more battery like a G-35 for starting then two smaller Odyssey batteries will give you the same start power for less weight. And if you are as paranoid as you sound then an old fashion gang switch for the system inter connect with a safety strap for you will keep the system disconnected in flight. As for your following statements about reliability, almost everything works without failure if properly maintained. The electrical system is in my experience the most under maintained system in an airplane. How many Cessna's have you looked at where ALL of the switches are 30 plus years old. The simple fact is that most people don't do anything to an electrical system until something fails. As far as fail proof, I fly airplanes of all types; little, middle, and big over 800 hours a year and so far I have not experienced a total electrical failure to a dark plane. As for the P-mag, I recovered an RV-7 from a highway two weekends ago when Both P-mags failed. Guess what, the electrical system worked perfectly...... Mike Larkin ATP MEL, Com SEL, Many Types Rat., A&P, & IE Lancair Legacy Build and Flown by Me TS-11 Iskra Restored and Flown by Me Kitfox IV re-engined and Flown by Me A320/319 Flown by Me.... Ps- I only get this way with very very closed minded people..... -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Tuesday, February 20, 2007 7:47 AM Subject: Re: Engines-List: Engine Running Rough An interesting opinion, not based in fact. A dual electrical system requires two alternators(heavier than a vacuum pump and one alternator), two batteries(Significant extra wt), two totally separate buses. If you interconnect them, you leave the possibility of one failure taking out both systems. If you don't interconnect you have to be able to live with what is on either bus by itself, which means you will need some additional duplication. That is not simpler, nor less complex. I have yet to see a failure-proof electrical system. Better to have enough to keep flying when(not if) the electrics fail. I have yet to see a CDI system that is more reliable than properly maintained magnetos, in 35 years of flying and maintaining aircraft and autos. The P-Mag/Emag(and others) may change that, eventually. They have been talking certification for several years. Prism from GAMI holds a lot of promise when it gets certified. The main mag failures you see are when folks try to skimp and run magnetos 1000+ hours without service. They should be opened and inspected every 500 hours. Sometimes folks have to relearn hard lessons all over again. You are free to do that with experimental aircraft. KM A&P/IA CP ASMEL-I -- 2/8/2007 ________________________________________________________________________________
Date: Feb 20, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Engine Running Rough
Mike, Unlike you, I'm not trying to persuade anyone that one system is better than the other. I've stated anyone can select what they want in experimental and make their own judgements. However, I flew for over 20 years in the Alaskan bush. That colors my opinion. I don't have any reason to fly a GA plane routinely in hard IFR(I choose not to fly for hire)...that also colors my opinion of electric systems. Gee...2 Pmags fail in flight...who da thunkit! Again, Pmag isn't available for 6 cylinders. Fact.......last I checked Barrett Precsion Engines would not supply an engine with electronic ignition, and their dyno tests showed less horsepower and hotter CHT with electronic ignition(IIRC). (they've built and tested more engines in a year than anyone here will in a lifetime). I'm open to the idea, but not impressed with the current products on the market. I just was refuting the claim by someone else that CD or other EI was better than dual mags. Yes, you can minimize the weight of two electrical systems, but it still is more complex than a single system with a vacuum pump powering one gyro, and if it makes you feel better you can add a second electric AI. I have experienced total electric failure in two different aircraft in flight and others on the ground, on well maintained aircraft. Zero vacuum pump failures. Everyone has different exeriences There also is some very careful testing of electronic ignition against dual mags on the Cafe400 website..well instrumented, etc. For the narrow spectrum of high altitude, less than 70% power, dual EI showed some added speed and fuel economy, at the expense of higher CHT. For all higher power power and altitudes below 10,000 ft, the dual mags were superior in all instances. http://cafefoundation.org/v2/research_reports.php On 2/20/07, Mike wrote: > > Kelly, > > If you use have a dual electrical system it requires two alternators > yes. A small 20 amp B&C alternator is very close to the weight of a > vacuum pump, drive, regulator, and required plumbing. And the B&C > alternator in my very small 13,000+ hours of flying and my 30 year of > aircraft maintenance shows the it should be much more reliable. If you > need a 30 amp hour or more battery like a G-35 for starting then two > smaller Odyssey batteries will give you the same start power for less > weight. And if you are as paranoid as you sound then an old fashion > gang switch for the system inter connect with a safety strap for you > will keep the system disconnected in flight. As for your following > statements about reliability, almost everything works without failure if > properly maintained. The electrical system is in my experience the most > under maintained system in an airplane. How many Cessna's have you > looked at where ALL of the switches are 30 plus years old. The simple > fact is that most people don't do anything to an electrical system until > something fails. As far as fail proof, I fly airplanes of all types; > little, middle, and big over 800 hours a year and so far I have not > experienced a total electrical failure to a dark plane. As for the > P-mag, I recovered an RV-7 from a highway two weekends ago when Both > P-mags failed. Guess what, the electrical system worked perfectly...... > > Mike Larkin > > ATP MEL, Com SEL, Many Types Rat., A&P, & IE > > Lancair Legacy Build and Flown by Me > TS-11 Iskra Restored and Flown by Me > Kitfox IV re-engined and Flown by Me > A320/319 Flown by Me.... > > Ps- I only get this way with very very closed minded people..... > > > -----Original Message----- > From: owner-engines-list-server(at)matronics.com > [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Kelly > McMullen > Sent: Tuesday, February 20, 2007 7:47 AM > To: engines-list(at)matronics.com > Subject: Re: Engines-List: Engine Running Rough > > > An interesting opinion, not based in fact. A dual electrical system > requires two alternators(heavier than a vacuum pump and one > alternator), two batteries(Significant extra wt), two totally separate > buses. If you interconnect them, you leave the possibility of one > failure taking out both systems. If you don't interconnect you have to > be able to live with what is on either bus by itself, which means you > will need some additional duplication. That is not simpler, nor less > complex. I have yet to see a failure-proof electrical system. Better > to have enough to keep flying when(not if) the electrics fail. > I have yet to see a CDI system that is more reliable than properly > maintained magnetos, in 35 years of flying and maintaining aircraft > and autos. The P-Mag/Emag(and others) may change that, eventually. > They have been talking certification for several years. Prism from > GAMI holds a lot of promise when it gets certified. > The main mag failures you see are when folks try to skimp and run > magnetos 1000+ hours without service. They should be opened and > inspected every 500 hours. Sometimes folks have to relearn hard > lessons all over again. You are free to do that with experimental > aircraft. > KM > A&P/IA > CP ASMEL-I > > -- > 2/8/2007 > > ________________________________________________________________________________
From: NYTerminat(at)aol.com
Date: Feb 20, 2007
Subject: Re: Battery choice
Peter, I'm using a Odyssey 680 for my 912ULS and am quite pleased with it. I have been flying up to the middle of January, now I am snowed in. Bob Spudis In a message dated 2/20/2007 10:42:50 A.M. Eastern Standard Time, peterc(at)pipcom.com writes: In the experimental environment for the average low tech, low power (but also low temp winters) requirements (Rotax 912S 100hp), is the extra expense of the RG batteries worth it? I once put an Odyssey 680 in a Mazda 13b aircraft replacing a cheap utility battery and wasn't all that impressed with cranking capacity and shelf life. When a friend wanted to order a larger RG for his 210 the local flying club maintenance guy said they tried them in their school aircraft and also didn't stay with them. What is the data on these batteries? Is "Immobilized electrolyte" the same as Recombinant gas? Thanks Peter


**************************************
Check out free AOL at http://free.aol.com/thenewaol/index.adp. Most comprehensive set of free safety and security tools, millions of free high-quality videos from across the web, free AOL Mail and much more. ________________________________________________________________________________
From: "Mike" <mlas(at)cox.net>
Subject: Engine Running Rough
Date: Feb 20, 2007
Frank, To the best of my knowledge you are correct. One of the P-mags came off time for some unknown reason (we think induced by temperature) and the other was along for the ride. Mike -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Hinde, Frank George (Corvallis) Sent: Tuesday, February 20, 2007 11:29 AM Subject: RE: Engines-List: Engine Running Rough Hello Mike, If this is the same incident I don't think the Pmags actually both failed, although the effect was similar. What I think probably happened was the timing on one of the P mags went way advanced. In this scenario the second Pmag is just along for the ride, i.e it sparks but the charge has already been lit at that point and hence doesn't do anything. This is still the subject of investigation as we speak...I certainly hope they find it 'cus I run Pmags myself. I think kelly's point was that the traditional magnetoes are more reliable than Pmags. Frank -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Mike Sent: Tuesday, February 20, 2007 9:51 AM Subject: RE: Engines-List: Engine Running Rough Kelly, If you use have a dual electrical system it requires two alternators yes. A small 20 amp B&C alternator is very close to the weight of a vacuum pump, drive, regulator, and required plumbing. And the B&C alternator in my very small 13,000+ hours of flying and my 30 year of aircraft maintenance shows the it should be much more reliable. If you need a 30 amp hour or more battery like a G-35 for starting then two smaller Odyssey batteries will give you the same start power for less weight. And if you are as paranoid as you sound then an old fashion gang switch for the system inter connect with a safety strap for you will keep the system disconnected in flight. As for your following statements about reliability, almost everything works without failure if properly maintained. The electrical system is in my experience the most under maintained system in an airplane. How many Cessna's have you looked at where ALL of the switches are 30 plus years old. The simple fact is that most people don't do anything to an electrical system until something fails. As far as fail proof, I fly airplanes of all types; little, middle, and big over 800 hours a year and so far I have not experienced a total electrical failure to a dark plane. As for the P-mag, I recovered an RV-7 from a highway two weekends ago when Both P-mags failed. Guess what, the electrical system worked perfectly...... Mike Larkin ATP MEL, Com SEL, Many Types Rat., A&P, & IE Lancair Legacy Build and Flown by Me TS-11 Iskra Restored and Flown by Me Kitfox IV re-engined and Flown by Me A320/319 Flown by Me.... Ps- I only get this way with very very closed minded people..... -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Tuesday, February 20, 2007 7:47 AM Subject: Re: Engines-List: Engine Running Rough An interesting opinion, not based in fact. A dual electrical system requires two alternators(heavier than a vacuum pump and one alternator), two batteries(Significant extra wt), two totally separate buses. If you interconnect them, you leave the possibility of one failure taking out both systems. If you don't interconnect you have to be able to live with what is on either bus by itself, which means you will need some additional duplication. That is not simpler, nor less complex. I have yet to see a failure-proof electrical system. Better to have enough to keep flying when(not if) the electrics fail. I have yet to see a CDI system that is more reliable than properly maintained magnetos, in 35 years of flying and maintaining aircraft and autos. The P-Mag/Emag(and others) may change that, eventually. They have been talking certification for several years. Prism from GAMI holds a lot of promise when it gets certified. The main mag failures you see are when folks try to skimp and run magnetos 1000+ hours without service. They should be opened and inspected every 500 hours. Sometimes folks have to relearn hard lessons all over again. You are free to do that with experimental aircraft. KM A&P/IA CP ASMEL-I -- 2/8/2007 -- 2/8/2007 -- 2/8/2007 ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Auto plugs
Date: Feb 20, 2007
One of th4 things I've never tried to do is replace the plugs on a plane with anything other than the same type of plugs that came off. Generally we used to inspect and clean the plugs every 50 hr. (commercial) and return them to service. At better than $50.00 a pop we weren't too interested in swapping plugs at the drop of a hat. the one rule we did use was if we dropped a plug, the never happened, the second drop would be in the oval filing cabinet. Good stuff but not why I'm replying... As I said I never replaced a plug with anything but the same type. so I am wondering if the thread and reach of an automotive plug will even fit into the hole?? Noel -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Wayne Sweet Sent: Tuesday, February 20, 2007 11:30 AM Subject: Re: Engines-List: Auto plugs First problem, the ignition harness will not work with auto plugs. To make things simple, just get LSE's CDI dual system, Dynon EFIS D10A or whatever EFIS you like and be done with "the Past". Wayne ----- Original Message ----- From: Bob <mailto:rfg842(at)cox.net> Sent: Tuesday, February 20, 2007 5:44 AM Subject: Engines-List: Auto plugs Didn't have time to read all of the last comments but how does an engine act with firing auto plugs with a magneto? At the cost of aviation shielded plugs, changing to auto plugs is an incentive. Any need to change plug gaps? Bob, Wichita <http://www.incredimail.com/index.asp?id=96917> Add FUN to your email - CLICK HERE! href="http://www.matronics.com/Navigator?Engines-List">http://www.matro nics. com/Navigator?Engines-List href="http://forums.matronics.com">http://forums.matronics.com Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-virus/ ________________________________________________________________________________
Subject: Auto plugs
Date: Feb 20, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
Need an adaptor and a standard 3/4" auto plugs fit Lycomings. Frank ________________________________ From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Noel Loveys Sent: Tuesday, February 20, 2007 3:25 PM Subject: RE: Engines-List: Auto plugs One of th4 things I've never tried to do is replace the plugs on a plane with anything other than the same type of plugs that came off. Generally we used to inspect and clean the plugs every 50 hr. (commercial) and return them to service. At better than $50.00 a pop we weren't too interested in swapping plugs at the drop of a hat. the one rule we did use was if we dropped a plug, the never happened, the second drop would be in the oval filing cabinet. Good stuff but not why I'm replying... As I said I never replaced a plug with anything but the same type. so I am wondering if the thread and reach of an automotive plug will even fit into the hole?? Noel -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Wayne Sweet Sent: Tuesday, February 20, 2007 11:30 AM To: engines-list(at)matronics.com Subject: Re: Engines-List: Auto plugs First problem, the ignition harness will not work with auto plugs. To make things simple, just get LSE's CDI dual system, Dynon EFIS D10A or whatever EFIS you like and be done with "the Past". Wayne ----- Original Message ----- From: Bob <mailto:rfg842(at)cox.net> To: engines-list(at)matronics.com Sent: Tuesday, February 20, 2007 5:44 AM Subject: Engines-List: Auto plugs Didn't have time to read all of the last comments but how does an engine act with firing auto plugs with a magneto? At the cost of aviation shielded plugs, changing to auto plugs is an incentive. Any need to change plug gaps? Bob, Wichita Add FUN to your email - CLICK HERE! <http://www.incredimail.com/index.asp?id=96917> href="http://www.matronics.com/Navigator?Engines-List">http://www.matro n ics.com/Navigator?Engines-List href="http://forums.matronics.com">http://forums.matronics.com href="http://www.matronics.com/Navigator?Engines-List">http://www.matro n ics.com/Navigator?Engines-List href="http://forums.matronics.com">http://forums.matronics.com Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-virus/ ________________________________________________________________________________
From: "steve korney" <s_korney(at)hotmail.com>
Subject: Engine Running Rough
Date: Feb 21, 2007
To the best of my knowledge you are correct. One of the P-mags came off time for some unknown reason..... That's not good to hear.....If they knew the reason, they could fix it....If they don't know the reason .... Well, then what? Best... Steve ----Original Message Follows---- From: "Mike" <mlas(at)cox.net> Subject: RE: Engines-List: Engine Running Rough Date: Tue, 20 Feb 2007 14:00:21 -0700 Frank, To the best of my knowledge you are correct. One of the P-mags came off time for some unknown reason (we think induced by temperature) and the other was along for the ride. Mike -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Hinde, Frank George (Corvallis) Sent: Tuesday, February 20, 2007 11:29 AM Subject: RE: Engines-List: Engine Running Rough Hello Mike, If this is the same incident I don't think the Pmags actually both failed, although the effect was similar. What I think probably happened was the timing on one of the P mags went way advanced. In this scenario the second Pmag is just along for the ride, i.e it sparks but the charge has already been lit at that point and hence doesn't do anything. This is still the subject of investigation as we speak...I certainly hope they find it 'cus I run Pmags myself. I think kelly's point was that the traditional magnetoes are more reliable than Pmags. Frank -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Mike Sent: Tuesday, February 20, 2007 9:51 AM Subject: RE: Engines-List: Engine Running Rough Kelly, If you use have a dual electrical system it requires two alternators yes. A small 20 amp B&C alternator is very close to the weight of a vacuum pump, drive, regulator, and required plumbing. And the B&C alternator in my very small 13,000+ hours of flying and my 30 year of aircraft maintenance shows the it should be much more reliable. If you need a 30 amp hour or more battery like a G-35 for starting then two smaller Odyssey batteries will give you the same start power for less weight. And if you are as paranoid as you sound then an old fashion gang switch for the system inter connect with a safety strap for you will keep the system disconnected in flight. As for your following statements about reliability, almost everything works without failure if properly maintained. The electrical system is in my experience the most under maintained system in an airplane. How many Cessna's have you looked at where ALL of the switches are 30 plus years old. The simple fact is that most people don't do anything to an electrical system until something fails. As far as fail proof, I fly airplanes of all types; little, middle, and big over 800 hours a year and so far I have not experienced a total electrical failure to a dark plane. As for the P-mag, I recovered an RV-7 from a highway two weekends ago when Both P-mags failed. Guess what, the electrical system worked perfectly...... Mike Larkin ATP MEL, Com SEL, Many Types Rat., A&P, & IE Lancair Legacy Build and Flown by Me TS-11 Iskra Restored and Flown by Me Kitfox IV re-engined and Flown by Me A320/319 Flown by Me.... Ps- I only get this way with very very closed minded people..... -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Tuesday, February 20, 2007 7:47 AM Subject: Re: Engines-List: Engine Running Rough An interesting opinion, not based in fact. A dual electrical system requires two alternators(heavier than a vacuum pump and one alternator), two batteries(Significant extra wt), two totally separate buses. If you interconnect them, you leave the possibility of one failure taking out both systems. If you don't interconnect you have to be able to live with what is on either bus by itself, which means you will need some additional duplication. That is not simpler, nor less complex. I have yet to see a failure-proof electrical system. Better to have enough to keep flying when(not if) the electrics fail. I have yet to see a CDI system that is more reliable than properly maintained magnetos, in 35 years of flying and maintaining aircraft and autos. The P-Mag/Emag(and others) may change that, eventually. They have been talking certification for several years. Prism from GAMI holds a lot of promise when it gets certified. The main mag failures you see are when folks try to skimp and run magnetos 1000+ hours without service. They should be opened and inspected every 500 hours. Sometimes folks have to relearn hard lessons all over again. You are free to do that with experimental aircraft. KM A&P/IA CP ASMEL-I -- 2/8/2007 -- 2/8/2007 -- 2/8/2007 _________________________________________________________________ Mortgage rates as low as 4.625% - Refinance $150,000 loan for $579 a month. Intro*Terms http://www.NexTag.com ________________________________________________________________________________
From: "steve korney" <s_korney(at)hotmail.com>
Subject: Auto plugs
Date: Feb 21, 2007
Some of the newer Lycoming cylinders are made to accept the 3/4 reach 14 MM auto plugs..... Best... Steve ----Original Message Follows---- From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com> Subject: RE: Engines-List: Auto plugs Date: Tue, 20 Feb 2007 23:41:44 -0000 Need an adaptor and a standard 3/4" auto plugs fit Lycomings. Frank ________________________________ From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Noel Loveys Sent: Tuesday, February 20, 2007 3:25 PM Subject: RE: Engines-List: Auto plugs One of th4 things I've never tried to do is replace the plugs on a plane with anything other than the same type of plugs that came off. Generally we used to inspect and clean the plugs every 50 hr. (commercial) and return them to service. At better than $50.00 a pop we weren't too interested in swapping plugs at the drop of a hat. the one rule we did use was if we dropped a plug, the never happened, the second drop would be in the oval filing cabinet. Good stuff but not why I'm replying... As I said I never replaced a plug with anything but the same type. so I am wondering if the thread and reach of an automotive plug will even fit into the hole?? Noel -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Wayne Sweet Sent: Tuesday, February 20, 2007 11:30 AM To: engines-list(at)matronics.com Subject: Re: Engines-List: Auto plugs First problem, the ignition harness will not work with auto plugs. To make things simple, just get LSE's CDI dual system, Dynon EFIS D10A or whatever EFIS you like and be done with "the Past". Wayne ----- Original Message ----- From: Bob <mailto:rfg842(at)cox.net> To: engines-list(at)matronics.com Sent: Tuesday, February 20, 2007 5:44 AM Subject: Engines-List: Auto plugs Didn't have time to read all of the last comments but how does an engine act with firing auto plugs with a magneto? At the cost of aviation shielded plugs, changing to auto plugs is an incentive. Any need to change plug gaps? Bob, Wichita Add FUN to your email - CLICK HERE! <http://www.incredimail.com/index.asp?id'917> href="http://www.matronics.com/Navigator?Engines-List">http://www.matron ics.com/Navigator?Engines-List href="http://forums.matronics.com">http://forums.matronics.com href="http://www.matronics.com/Navigator?Engines-List">http://www.matron ics.com/Navigator?Engines-List href="http://forums.matronics.com">http://forums.matronics.com Checked by PC Tools AntiVirus (3.1.0.10 - 9.061.014). http://www.pctools.com/anti-virus/ _________________________________________________________________ Refi Now: Rates near 39yr lows! $430,000 Mortgage for $1,399/mo - Calculate new payment ________________________________________________________________________________
Subject: Engine Running Rough
Date: Feb 21, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
They may not know for absolute sure but there is a failure mode they found that allows the unit with certain software versions to lose its timing. There is a sevice bulletin on the Emag website about it. It certainly makes sense and fits the description of the issues on the downed airplane. I also had the same issues but my engine did not actually quit. Frank -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of steve korney Sent: Tuesday, February 20, 2007 4:34 PM Subject: RE: Engines-List: Engine Running Rough --> To the best of my knowledge you are correct. One of the P-mags came off time for some unknown reason..... That's not good to hear.....If they knew the reason, they could fix it....If they don't know the reason .... Well, then what? Best... Steve ----Original Message Follows---- From: "Mike" <mlas(at)cox.net> Subject: RE: Engines-List: Engine Running Rough Date: Tue, 20 Feb 2007 14:00:21 -0700 Frank, To the best of my knowledge you are correct. One of the P-mags came off time for some unknown reason (we think induced by temperature) and the other was along for the ride. Mike -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Hinde, Frank George (Corvallis) Sent: Tuesday, February 20, 2007 11:29 AM Subject: RE: Engines-List: Engine Running Rough Hello Mike, If this is the same incident I don't think the Pmags actually both failed, although the effect was similar. What I think probably happened was the timing on one of the P mags went way advanced. In this scenario the second Pmag is just along for the ride, i.e it sparks but the charge has already been lit at that point and hence doesn't do anything. This is still the subject of investigation as we speak...I certainly hope they find it 'cus I run Pmags myself. I think kelly's point was that the traditional magnetoes are more reliable than Pmags. Frank -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Mike Sent: Tuesday, February 20, 2007 9:51 AM Subject: RE: Engines-List: Engine Running Rough Kelly, If you use have a dual electrical system it requires two alternators yes. A small 20 amp B&C alternator is very close to the weight of a vacuum pump, drive, regulator, and required plumbing. And the B&C alternator in my very small 13,000+ hours of flying and my 30 year of aircraft maintenance shows the it should be much more reliable. If you need a 30 amp hour or more battery like a G-35 for starting then two smaller Odyssey batteries will give you the same start power for less weight. And if you are as paranoid as you sound then an old fashion gang switch for the system inter connect with a safety strap for you will keep the system disconnected in flight. As for your following statements about reliability, almost everything works without failure if properly maintained. The electrical system is in my experience the most under maintained system in an airplane. How many Cessna's have you looked at where ALL of the switches are 30 plus years old. The simple fact is that most people don't do anything to an electrical system until something fails. As far as fail proof, I fly airplanes of all types; little, middle, and big over 800 hours a year and so far I have not experienced a total electrical failure to a dark plane. As for the P-mag, I recovered an RV-7 from a highway two weekends ago when Both P-mags failed. Guess what, the electrical system worked perfectly...... Mike Larkin ATP MEL, Com SEL, Many Types Rat., A&P, & IE Lancair Legacy Build and Flown by Me TS-11 Iskra Restored and Flown by Me Kitfox IV re-engined and Flown by Me A320/319 Flown by Me.... Ps- I only get this way with very very closed minded people..... -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Kelly McMullen Sent: Tuesday, February 20, 2007 7:47 AM Subject: Re: Engines-List: Engine Running Rough An interesting opinion, not based in fact. A dual electrical system requires two alternators(heavier than a vacuum pump and one alternator), two batteries(Significant extra wt), two totally separate buses. If you interconnect them, you leave the possibility of one failure taking out both systems. If you don't interconnect you have to be able to live with what is on either bus by itself, which means you will need some additional duplication. That is not simpler, nor less complex. I have yet to see a failure-proof electrical system. Better to have enough to keep flying when(not if) the electrics fail. I have yet to see a CDI system that is more reliable than properly maintained magnetos, in 35 years of flying and maintaining aircraft and autos. The P-Mag/Emag(and others) may change that, eventually. They have been talking certification for several years. Prism from GAMI holds a lot of promise when it gets certified. The main mag failures you see are when folks try to skimp and run magnetos 1000+ hours without service. They should be opened and inspected every 500 hours. Sometimes folks have to relearn hard lessons all over again. You are free to do that with experimental aircraft. KM A&P/IA CP ASMEL-I -- 2/8/2007 -- 2/8/2007 -- 2/8/2007 _________________________________________________________________ Mortgage rates as low as 4.625% - Refinance $150,000 loan for $579 a month. Intro*Terms http://www.NexTag.com ________________________________________________________________________________
From: "Mike" <mlas(at)cox.net>
Subject: Auto plugs
Date: Feb 20, 2007
My Light Speed system on my IO-550 uses auto plugs=85.. I change them every 100 hours at $40 a set.. Mike -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Noel Loveys Sent: Tuesday, February 20, 2007 4:25 PM Subject: RE: Engines-List: Auto plugs One of th4 things I've never tried to do is replace the plugs on a plane with anything other than the same type of plugs that came off. Generally we used to inspect and clean the plugs every 50 hr. (commercial) and return them to service. At better than $50.00 a pop we weren't too interested in swapping plugs at the drop of a hat. the one rule we did use was if we dropped a plug, the never happened, the second drop would be in the oval filing cabinet. Good stuff but not why I'm replying... As I said I never replaced a plug with anything but the same type. so I am wondering if the thread and reach of an automotive plug will even fit into the hole?? -- 2/8/2007 -- 2/8/2007 ________________________________________________________________________________
From: "Mike" <mlas(at)cox.net>
Subject: Engine Running Rough
Date: Feb 20, 2007
Frank. The airplane engine didn't quit. The CHT's and EGT's went off the chart and the engine couldn't make enough power to maintain altitude. At the time the plane was in the high mountains in east AZ. Mike -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Hinde, Frank George (Corvallis) Sent: Tuesday, February 20, 2007 6:20 PM Subject: RE: Engines-List: Engine Running Rough They may not know for absolute sure but there is a failure mode they found that allows the unit with certain software versions to lose its timing. There is a sevice bulletin on the Emag website about it. It certainly makes sense and fits the description of the issues on the downed airplane. I also had the same issues but my engine did not actually quit. Frank -- 2/8/2007 ________________________________________________________________________________
From: "Neal George" <neal.george(at)mchsi.com>
Subject: Engine Running Rough
Date: Feb 20, 2007
Steve - I must disagree. I called EMagAir last week to ask some unrelated questions about the EMag and PMag that are hanging on my engine. After answering my questions (harness related) and discussing the background, I asked Brad to tell me what he knew about this incident. He explained that they had examined and tested the suspect units and could not duplicate the failure on the test stand. If I understood him correctly, rather than send the suspect units back to the owner, he kept them for further testing and returned new PMags. I find that refreshing and distinctly responsible, rather than typical and disturbing. And I'm keeping my EMag/PMag setup (unless I find a wad of $20s in the laundry that will allow me to upgrade to twin PMags). Neal RV-7 N8ZG _still_ wiring Neal E. George 2023 Everglades Drive Navarre, FL 32566 Home - 850-515-0640 Cell - 850-218-4838 --> To the best of my knowledge you are correct. One of the P-mags came off time for some unknown reason..... That's not good to hear.....If they knew the reason, they could fix it....If they don't know the reason .... Well, then what? Best... Steve ________________________________________________________________________________
Subject: Engine Running Rough
Date: Feb 21, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
Thanks for the clarification Mike. Seems our Pmag issues were pretty much identical then. Frank -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Mike Sent: Tuesday, February 20, 2007 5:31 PM Subject: RE: Engines-List: Engine Running Rough Frank. The airplane engine didn't quit. The CHT's and EGT's went off the chart and the engine couldn't make enough power to maintain altitude. At the time the plane was in the high mountains in east AZ. Mike -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Hinde, Frank George (Corvallis) Sent: Tuesday, February 20, 2007 6:20 PM Subject: RE: Engines-List: Engine Running Rough They may not know for absolute sure but there is a failure mode they found that allows the unit with certain software versions to lose its timing. There is a sevice bulletin on the Emag website about it. It certainly makes sense and fits the description of the issues on the downed airplane. I also had the same issues but my engine did not actually quit. Frank -- 2/8/2007 ________________________________________________________________________________
From: "Mike" <mlas(at)cox.net>
Subject: Engine Running Rough
Date: Feb 21, 2007
Well, when we ran the airplane on the side of the road for 30 minutes we couldn't duplicate the problem, everything was working great. So we flew it out thinking it was fuel ice, the airplane pressed on to Phoenix. It wasn't until the third flight that it happened again (as explained to me). Just because you can't duplicate a failure on the bench doesn't mean it didn't happen. One thing to always remember with certified stuff, if it fails there is an AD in your future. We are the AD process in the experimental world. Turn key operators need not apply. Mike Larkin -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Neal George Sent: Tuesday, February 20, 2007 7:05 PM Subject: RE: Engines-List: Engine Running Rough Steve - I must disagree. I called EMagAir last week to ask some unrelated questions about the EMag and PMag that are hanging on my engine. After answering my questions (harness related) and discussing the background, I asked Brad to tell me what he knew about this incident. He explained that they had examined and tested the suspect units and could not duplicate the failure on the test stand. If I understood him correctly, rather than send the suspect units back to the owner, he kept them for further testing and returned new PMags. Remember the folks over at P-mag don't like bad news. Don marry a product, help make it better. -- 2/8/2007 ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Engine Running Rough
Date: Feb 21, 2007
Electronics techs call then Intermittent problems....very hard to diagnose. Noel > -----Original Message----- > From: owner-engines-list-server(at)matronics.com > [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Mike > Sent: Wednesday, February 21, 2007 11:28 AM > To: engines-list(at)matronics.com > Subject: RE: Engines-List: Engine Running Rough > > > > Well, when we ran the airplane on the side of the road for 30 > minutes we > couldn't duplicate the problem, everything was working great. So we > flew it out thinking it was fuel ice, the airplane pressed on to > Phoenix. It wasn't until the third flight that it happened again (as > explained to me). Just because you can't duplicate a failure on the > bench doesn't mean it didn't happen. One thing to always > remember with > certified stuff, if it fails there is an AD in your future. > We are the > AD process in the experimental world. Turn key operators need > not apply. > > Mike Larkin > > -----Original Message----- > From: owner-engines-list-server(at)matronics.com > [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Neal > George > Sent: Tuesday, February 20, 2007 7:05 PM > To: engines-list(at)matronics.com > Subject: RE: Engines-List: Engine Running Rough > > > > Steve - > > I must disagree. I called EMagAir last week to ask some unrelated > questions > about the EMag and PMag that are hanging on my engine. After > answering > my > questions (harness related) and discussing the background, I > asked Brad > to > tell me what he knew about this incident. He explained that they had > examined and tested the suspect units and could not duplicate the > failure on > the test stand. If I understood him correctly, rather than send the > suspect > units back to the owner, he kept them for further testing and returned > new > PMags. > > Remember the folks over at P-mag don't like bad news. Don marry a > product, help make it better. > > -- > 2/8/2007 > > > > > > ________________________________________________________________________________
Date: Feb 22, 2007
From: "Bob" <rfg842(at)cox.net>
Subject: Auto plugs
Just as a matter of interest, Great Plains, Boys Town, NE, does offer an adapter for a shielded harness to auto plugs. Have not used them but it' s a great idea. Bob, Wichita ________________________________________________________________________________
From: GENTRYLL(at)aol.com
Date: Feb 23, 2007
Subject: Lycoming Experts
Would some of you guys that know a lot about Lycomings explain what some of the engines have in common. Like the O-235, O-290, O-320. You see things on the net like O-290 converted to O-320, How is that done. What crankshafts some of the engines share. What cylinders are interchangeable. I have read that some of the engines such as the O-290 and O-435 share common cylinders, jut more of them.


**************************************
AOL now offers free email to everyone. Find out more about what's free from AOL at http://www.aol.com. ________________________________________________________________________________
Subject: Lycoming Experts
Date: Feb 23, 2007
From: "Monty Barrett Sr" <MONTY(at)bpaengines.com>
Some cylinders interchange: Parallel valve 360-540, WD to WD, ND to ND Angle head 360 to 540 t0 720, WD to WD, ND to ND AH 480 cyls will fit 320 but other considerations are required 290's will NOT convert o 320 sucessfully. If you throw enough money at it I suppose it could happen 235 C engines will not successfully convert to later series, such as L2C, F2C, BUT I have done it specifically for 1 airplane. Not approved. It is the Knight Twister that won best plans built airplane at OSH about 4 years ago. Built by Hale Wallace. Hale stated he wanted 130 HP at 3000 RPM and I got it. Used 0-235-F2C cylinder assemblies on 0-235 C cases, machined cases for 7/16 TCM thrubolts. 0-320 can be and have been converted to 360's many times. Expensive because of the crank and rods required. But it is relatively easy from the standpoint of assembly. Almost any 0- engine can be converted to I0. Need to have the fuel pump drive. These are brief highlights. Not meant to be a conversion manual. Use at your own risk. Monty Barrett -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of GENTRYLL(at)aol.com Sent: Friday, February 23, 2007 7:47 AM Subject: Engines-List: Lycoming Experts Would some of you guys that know a lot about Lycomings explain what some of the engines have in common. Like the O-235, O-290, O-320. You see things on the net like O-290 converted to O-320, How is that done. What crankshafts some of the engines share. What cylinders are interchangeable. I have read that some of the engines such as the O-290 and O-435 share common cylinders, jut more of them. ________________________________ AOL now offers free email to everyone. Find out more about what's f241x4298082137/aol?redir=http://www.aol.com" l ?redir=http%3A%2F%2Fwww%2Eaol%2Ecom" target="_blank">AOL.com. ________________________________________________________________________________
From: "jrc" <jrccea(at)bellsouth.net>
Subject: Re: Lycoming Experts
Date: Feb 23, 2007
http://home.adelphia.net/~aeroengine/Lycoming.html ----- Original Message ----- From: GENTRYLL(at)aol.com To: engines-list(at)matronics.com Sent: Friday, February 23, 2007 7:47 AM Subject: Engines-List: Lycoming Experts Would some of you guys that know a lot about Lycomings explain what some of the engines have in common. Like the O-235, O-290, O-320. You see things on the net like O-290 converted to O-320, How is that done. What crankshafts some of the engines share. What cylinders are interchangeable. I have read that some of the engines such as the O-290 and O-435 share common cylinders, jut more of them. ------------------------------------------------------------------------- ----- AOL now offers free email to everyone. Find out more about what's f241x4298082137/aol?redir=http://www.aol.com" l?redir=http%3A%2F%2Fwww%2Eaol%2Ecom" target="_blank">AOL.com. ________________________________________________________________________________
Subject: EA81 FI
From: "secatur" <appraise1(at)bigpond.com>
Date: Mar 05, 2007
Anybody out there have any experience with a fuel inj. EA81 (minusTurbo) I bought one for my CH701 which has a Wolf3dV4 ECU. Questions are..what injectors would be recommended (over stock) and does anyone know of anyone in West Australia who would be recommended for tuning. I'm trying to get manuals, but at this time Wolf3d's website just directs you to their store. Thanks, Steve Read this topic online here: http://forums.matronics.com/viewtopic.php?p=98793#98793 ________________________________________________________________________________
Subject: New Lycoming Website
From: "Jon A. Delamarter" <jdelamarter(at)lycoming.textron.com>
Date: Mar 13, 2007
Check out the new Lycoming website at www.lycoming.com. -------- Jon A. Delamarter Thunderbolt Manager Lycoming Engines Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100298#100298 ________________________________________________________________________________
Subject: Re: New Lycoming Website
Date: Mar 13, 2007
From: teamgrumman(at)aol.com
Is there any chance Lycoming could buy-out the LASAR portion of Unison/GE and make it work? It took me 10 months to get the correct controller and harness. Then, when I had questions, no one would return my calls. In fact, I never did get a call back from Steve Carter at Unison. I was never able to talk to anyone regarding the timing of the mags. -----Original Message----- From: jdelamarter(at)lycoming.textron.com Sent: Tue, 13 Mar 2007 9:57 AM Subject: Engines-List: New Lycoming Website Check out the new Lycoming website at www.lycoming.com. -------- Jon A. Delamarter Thunderbolt Manager Lycoming Engines Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100298#100298 ________________________________________________________________________ AOL now offers free email to everyone. Find out more about what's free from AOL at AOL.com. ________________________________________________________________________________
Subject: Re: New Lycoming Website
From: "Jon A. Delamarter" <jdelamarter(at)lycoming.textron.com>
Date: Mar 13, 2007
Gary: Thanks for your question. I'm not aware of any intitiative from Lycoming to procure any part of Unison's business. However, I am frequently in contact with Unison. I would like to forward your request to my contact, Fred Sontag. Please email me your concerns at jdelamarter(at)lycoming.textron.com. I willcommunicate with Fred and ask him for a response. I know from talking to him that he is working hard to close the loop on these types of concerns. He took care of one of my customers recently in an extremely effective manner. Regards, -------- Jon A. Delamarter Thunderbolt Manager Lycoming Engines Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100312#100312 ________________________________________________________________________________
Date: Mar 14, 2007
From: victor verdev <vjvus(at)yahoo.com>
Subject: Lycoming 0-235 Screen Oil Filter
I'm installing an the old style oil screen filter housing(69510) with internal screen on A used 0-235 LYC. The housing has the Temp Control oil cooler bypass valve(75944) installed in end of housing. Does (69510)housing bolt right onto the engines accessory housing, or does it need the steel adapter plate(LW-12999)between housing and engine? Get your own web address. http://smallbusiness.yahoo.com/domains/?p=BESTDEAL ________________________________________________________________________________
Subject: Re: New Lycoming Website
Date: Mar 14, 2007
From: teamgrumman(at)aol.com
Thanks for the response. I do firewall forward restorations on Grumman Tigers and Cheetahs about 3 or 4 times a year. About 50% of them ask for the LASAR mags and, quite frankly, I discourage it because of my experience with Unison. They, it appears to me and everyone else with whom I've talked, have no desire to produce this product. I get the impression that the LASAR mags are a nuisance to them. I would like to see Lycoming take the initiative and produce an electronic ignition for their engines. And do it a lot simpler than Unison. Right now there are several electronic ignitions on the market for experimental aircraft that are clean and simple; get one of them approved for certified aircraft. Gary -----Original Message----- From: jdelamarter(at)lycoming.textron.com Sent: Tue, 13 Mar 2007 11:04 AM Subject: Engines-List: Re: New Lycoming Website Gary: Thanks for your question. I'm not aware of any intitiative from Lycoming to procure any part of Unison's business. However, I am frequently in contact with Unison. I would like to forward your request to my contact, Fred Sontag. Please email me your concerns at jdelamarter(at)lycoming.textron.com. I willcommunicate with Fred and ask him for a response. I know from talking to him that he is working hard to close the loop on these types of concerns. He took care of one of my customers recently in an extremely effective manner. Regards, -------- Jon A. Delamarter Thunderbolt Manager Lycoming Engines Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100312#100312 ________________________________________________________________________ AOL now offers free email to everyone. Find out more about what's free from AOL at AOL.com. ________________________________________________________________________________
Date: Mar 14, 2007
From: Gilles Thesee <Gilles.Thesee@ac-grenoble.fr>
Subject: Fuel pump tests
Hi all, Just conducted some test on our Rotax 914 fuel system, just to learn more. The idea was running a brand new electrical pump with clear plastic tubing from different points of the circuit, and observing what was going on. We noted that slugs of bubbles appear on the suction side of the pump when it is connected downstream of the fuel valve (large pressure drop). On the pressure side of the pump, very few bubbles appear. My interpretation is that when the pump draws fuel from a restricted portion of the circuit such as the fuel valve and all the fittings and elbows, the most volatile fraction of the fuel tends to vaporise, and then condenses when under pressure downstream of the pump. I believe this is a normal phenomenon, but it was the first time I observed it through clear hoses. Has anyone already seen such a phenomenon ? Any comments ? Some info on our engine fuel system here : http://contrails.free.fr/engine_regul_en.php Thanks, Regards, Gilles Thesee http://contrails.free.fr ________________________________________________________________________________
Subject: Fuel pump tests
Date: Mar 14, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
Your right that is exactly what is happening. It also gets worse as the temperature of the fuel increases, namely thru a hot engine driven pump...I gets worse further with altitude and the harder you suck on the fuel. When it gets really bad its called vapour lock and your engine quits. It will also happen more with autofuel than with 100LL due to the higher vapour pressure of the mogas. Low wing airplanes (with wing tanks and no header tank are much more susceptable because the engine driven pump is sucking uphill. This coindiently may happen at the worse possible time i.e a hot Summer day at a high altitude airport where your fuel has been heat soaked....You run full power, the engine gets real hot and Here come the trees! So, what to do?....Mount a low pressure electric pump as close to the outlet of tha tank as possible with no pressure drop on the inlet side of the pump. My Zenair Zodiac (and my current Fuel injected RV 7) did not have an engine driven pump, just a Facet fuel pump in each wing root. Thus the pump always pushed on the fuel, never sucked. The pumps were (are) wired to independent circuits such that if a pump failed the other pump will take over. Lycomings typically have a low level booster pump to augment the engine driven pump and that's with 100LL. Frank RV7a no engine driven pump, mainly cus one day I want to use Mogas in it....but only below about 15,000feet. -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Gilles Thesee Sent: Wednesday, March 14, 2007 12:10 PM Subject: Engines-List: Fuel pump tests --> <Gilles.Thesee@ac-grenoble.fr> Hi all, Just conducted some test on our Rotax 914 fuel system, just to learn more. The idea was running a brand new electrical pump with clear plastic tubing from different points of the circuit, and observing what was going on. We noted that slugs of bubbles appear on the suction side of the pump when it is connected downstream of the fuel valve (large pressure drop). On the pressure side of the pump, very few bubbles appear. My interpretation is that when the pump draws fuel from a restricted portion of the circuit such as the fuel valve and all the fittings and elbows, the most volatile fraction of the fuel tends to vaporise, and then condenses when under pressure downstream of the pump. I believe this is a normal phenomenon, but it was the first time I observed it through clear hoses. Has anyone already seen such a phenomenon ? Any comments ? Some info on our engine fuel system here : http://contrails.free.fr/engine_regul_en.php Thanks, Regards, Gilles Thesee http://contrails.free.fr ________________________________________________________________________________
Subject: Re: New Lycoming Website
From: "Jon A. Delamarter" <jdelamarter(at)lycoming.textron.com>
Date: Mar 14, 2007
Gary: Actually, Lycoming is extensively engaged in Electronic Engine Control development. I can't spill the beans yet, but suffice to say that we are making excellent progress and I am really excited about the product we will be bringing to market! This system will control all engine parameters, not just ignition. Keep watching! All the best, -------- Jon A. Delamarter Thunderbolt Manager Lycoming Engines Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100596#100596 ________________________________________________________________________________
Subject: Re: New Lycoming Website
Date: Mar 15, 2007
From: teamgrumman(at)aol.com
Awesome. In what year? -----Original Message----- From: jdelamarter(at)lycoming.textron.com Sent: Wed, 14 Mar 2007 5:33 PM Subject: Engines-List: Re: New Lycoming Website Gary: Actually, Lycoming is extensively engaged in Electronic Engine Control development. I can't spill the beans yet, but suffice to say that we are making excellent progress and I am really excited about the product we will be bringing to market! This system will control all engine parameters, not just ignition. Keep watching! All the best, -------- Jon A. Delamarter Thunderbolt Manager Lycoming Engines Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100596#100596 ________________________________________________________________________ AOL now offers free email to everyone. Find out more about what's free from AOL at AOL.com. ________________________________________________________________________________
Subject: Re: New Lycoming Website
From: "Jon A. Delamarter" <jdelamarter(at)lycoming.textron.com>
Date: Mar 15, 2007
Again, I'm not at liberty to discuss development details, including timelines, but I can tell you that the EEC program is Lycoming's top new product development program. Our team of engineers and experimental technicians is working almost around the clock to complete the project. -------- Jon A. Delamarter Thunderbolt Manager Lycoming Engines Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100659#100659 ________________________________________________________________________________
Subject: Re: New Lycoming Website
From: "Jon A. Delamarter" <jdelamarter(at)lycoming.textron.com>
Date: Mar 15, 2007
Okay, Gary, here's the response from Unison. Hey John, Sounds to me like your customer got a bit of the "Unison shuffle". I can assure you and your customer Unison does not view LASAR as a nuisance, but as a premium product that requires a lot of hands on to "spec" out a complete system. We often ask questions that, to an end customer, may seem ridulous or uneccessary, but we require a lot of information to provide them with the exactly correct system. One of the major problems with LASAR is the complete lack of skilled individuals in the field with the LASAR systems. Unlike our Slick magnetos, LASAR is not a simple product. So many mechanics shy away from it, typically as it is not a simple product to understand. For that reason, all LASAR questions are now 100% answered by Unison, not by trained mechanics in the field. If we had to answer every single question about Slick mags, we'd be overloaded. So with LASAR, it's a crushing amount of interest handled by only one or two people at Unison. In fact, while we do not attempt to make excuses, our product support engineer of 45 years, Lyman Hardt, passed away last year. His loss has hurt Unison in many ways. Specifically, in our piston engine product support group. We lost more than a person, we lost a lifetime of experience. It sounds like here, your customer may have caught our product support person (yes, we only have one) on a bad day. We have not replaced Lyman at Unison and left 100% of his responsibilities to one person. While I may personally disagree with this strategy, it is what it is. What I recommend for your customers is to contact our piston engine product support line at 904-739-4081 first. We are adding a new (not really new, as he's been at Unison for almost 10 years) product support engineer in the next few weeks. If your end customers do not feel they are getting the support they require, feel free to have them contact our field reps as referenced below. I can assure you, Unison is not going anywhere. While we are not perfect, we strive to fix any perceived issues in a timely manner. Kinda like LASAR, which has undergone 4 revision upgrades in it's 12 year history, we put our money where our mouth is. By the way, you can tell your customer that the LASAR product line is for sale. What's he offering?... :) >From stormy New Zealand, Fred Sontag Unison Distribution Sales Manager Eastern US & Canada Kara Smith 904-739-4208 kara.smith(at)unisonindustries.com Western US & Canada Gina Van Slyke 904-739-4049 gina.van.slyke(at)unisonindustries.com Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100663#100663 ________________________________________________________________________________
Date: Mar 15, 2007
From: Gilles Thesee <Gilles.Thesee@ac-grenoble.fr>
Subject: Re: Fuel pump tests
Hinde, Frank George (Corvallis) a crit : > > > Your right that is exactly what is happening. It also gets worse as the > temperature of the fuel increases, namely thru a hot engine driven > pump...I gets worse further with altitude and the harder you suck on the > fuel. When it gets really bad its called vapour lock and your engine > quits. It will also happen more with autofuel than with 100LL due to the > higher vapour pressure of the mogas. Low wing airplanes (with wing tanks > and no header tank are much more susceptable because the engine driven > pump is sucking uphill. > > This coindiently may happen at the worse possible time i.e a hot Summer > day at a high altitude airport where your fuel has been heat > soaked....You run full power, the engine gets real hot and Here come the > trees! > > So, what to do?....Mount a low pressure electric pump as close to the > outlet of tha tank as possible with no pressure drop on the inlet side > of the pump. > Frank, Thank you for responding. Actually we have wing tanks and our pumps are on the firewall, some inches higher than wing root level. To date we've reached FL 145 in winter on Avgas, and recently flew at FL 135 on Mogas without any problems. I also flew at 37C OAT (only up to 6000 ft). But you're right on the pumps in the wing roots in a perfect circuit. Best regards, Gilles http://contrails.free.fr ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Fuel pump tests
Date: Mar 15, 2007
I use a siphon to defuel my plane after every flight. I made the siphon specifically out of clear fuel line and a squeeze bulb the squeeze bulb is considerably below the highest point on the siphon but it always seems to find a bubble or two while the fuel is flowing. If I stop the fuel flow by plugging the out flow the bubbles completely disappear to re appear again as soon as the fuel starts to flow again. Go figure. Noel > -----Original Message----- > From: owner-engines-list-server(at)matronics.com > [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of > Gilles Thesee > Sent: Wednesday, March 14, 2007 4:40 PM > To: engines-list(at)matronics.com > Subject: Engines-List: Fuel pump tests > > > <Gilles.Thesee@ac-grenoble.fr> > > Hi all, > > Just conducted some test on our Rotax 914 fuel system, just > to learn more. > The idea was running a brand new electrical pump with clear plastic > tubing from different points of the circuit, and observing what was > going on. > We noted that slugs of bubbles appear on the suction side of the pump > when it is connected downstream of the fuel valve (large > pressure drop). > On the pressure side of the pump, very few bubbles appear. > > My interpretation is that when the pump draws fuel from a restricted > portion of the circuit such as the fuel valve and all the > fittings and > elbows, the most volatile fraction of the fuel tends to vaporise, and > then condenses when under pressure downstream of the pump. > I believe this is a normal phenomenon, but it was the first time I > observed it through clear hoses. > Has anyone already seen such a phenomenon ? Any comments ? > > Some info on our engine fuel system here : > http://contrails.free.fr/engine_regul_en.php > > > Thanks, > Regards, > Gilles Thesee > http://contrails.free.fr > > > > > > > > > > > ________________________________________________________________________________
From: "Noel Loveys" <noelloveys(at)yahoo.ca>
Subject: Re: New Lycoming Website
Date: Mar 15, 2007
About time!!!!! Thanks. I'll be watching! What I'd like to see is a control by wire piston engine. One control for everything. Noel > -----Original Message----- > From: owner-engines-list-server(at)matronics.com > [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of > Jon A. Delamarter > Sent: Wednesday, March 14, 2007 10:04 PM > To: engines-list(at)matronics.com > Subject: Engines-List: Re: New Lycoming Website > > > > > Gary: > > Actually, Lycoming is extensively engaged in Electronic > Engine Control development. I can't spill the beans yet, but > suffice to say that we are making excellent progress and I am > really excited about the product we will be bringing to > market! This system will control all engine parameters, not > just ignition. Keep watching! > > All the best, > > -------- > Jon A. Delamarter > Thunderbolt Manager > Lycoming Engines > > > > > Read this topic online here: > > http://forums.matronics.com/viewtopic.php?p=100596#100596 > > > > > > > > > > > ________________________________________________________________________________
Subject: Re: New Lycoming Website
Date: Mar 16, 2007
From: teamgrumman(at)aol.com
is this something as straight forward (I say, tongue-in-cheek) to install as the LASAR? -----Original Message----- From: jdelamarter(at)lycoming.textron.com Sent: Thu, 15 Mar 2007 2:34 AM Subject: Engines-List: Re: New Lycoming Website Again, I'm not at liberty to discuss development details, including timelines, but I can tell you that the EEC program is Lycoming's top new product development program. Our team of engineers and experimental technicians is working almost around the clock to complete the project. -------- Jon A. Delamarter Thunderbolt Manager Lycoming Engines Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100659#100659 ________________________________________________________________________ AOL now offers free email to everyone. Find out more about what's free from AOL at AOL.com. ________________________________________________________________________________
Subject: Re: New Lycoming Website
Date: Mar 16, 2007
From: teamgrumman(at)aol.com
Thanks for the update. I printed the email, I'll save it for future installations. Hopefully, next time will go easier. -----Original Message----- From: jdelamarter(at)lycoming.textron.com Sent: Thu, 15 Mar 2007 4:10 AM Subject: Engines-List: Re: New Lycoming Website Okay, Gary, here's the response from Unison. Hey John, Sounds to me like your customer got a bit of the "Unison shuffle". I can assure you and your customer Unison does not view LASAR as a nuisance, but as a premium product that requires a lot of hands on to "spec" out a complete system. We often ask questions that, to an end customer, may seem ridulous or uneccessary, but we require a lot of information to provide them with the exactly correct system. One of the major problems with LASAR is the complete lack of skilled individuals in the field with the LASAR systems. Unlike our Slick magnetos, LASAR is not a simple product. So many mechanics shy away from it, typically as it is not a simple product to understand. For that reason, all LASAR questions are now 100% answered by Unison, not by trained mechanics in the field. If we had to answer every single question about Slick mags, we'd be overloaded. So with LASAR, it's a crushing amount of interest handled by only one or two people at Unison. In fact, while we do not attempt to make excuses, our product support engineer of 45 years, Lyman Hardt, passed away last year. His loss has hurt Unison in many ways. Specifically, in our piston engine product support group. We lost more than a person, we lost a lifetime of experience. It sounds like here, your customer may have caught our product support person (yes, we only have one) on a bad day. We have not replaced Lyman at Unison and left 100% of his responsibilities to one person. While I may personally disagree with this strategy, it is what it is. What I recommend for your customers is to contact our piston engine product support line at 904-739-4081 first. We are adding a new (not really new, as he's been at Unison for almost 10 years) product support engineer in the next few weeks. If your end customers do not feel they are getting the support they require, feel free to have them contact our field reps as referenced below. I can assure you, Unison is not going anywhere. While we are not perfect, we strive to fix any perceived issues in a timely manner. Kinda like LASAR, which has undergone 4 revision upgrades in it's 12 year history, we put our money where our mouth is. By the way, you can tell your customer that the LASAR product line is for sale. What's he offering?... :) >From stormy New Zealand, Fred Sontag Unison Distribution Sales Manager Eastern US & Canada Kara Smith 904-739-4208 kara.smith(at)unisonindustries.com Western US & Canada Gina Van Slyke 904-739-4049 gina.van.slyke(at)unisonindustries.com Read this topic online here: http://forums.matronics.com/viewtopic.php?p=100663#100663 ________________________________________________________________________ AOL now offers free email to everyone. Find out more about what's free from AOL at AOL.com. ________________________________________________________________________________
Subject: Fuel pump tests
Date: Mar 16, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
But didn't you say you saw bubbles with the clear hoses? This implies the onset of fuel boiling on the suction side of the pump. I guess my concern is if you saw bubbles on the ground then these bubbles are likely to be larger at the conditions I described. In other words my concern is you might be getting a little close to a true vapour lock situation. Cheers Frank -----Original Message----- From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of Gilles Thesee Sent: Thursday, March 15, 2007 1:17 PM Subject: Re: Engines-List: Fuel pump tests --> <Gilles.Thesee@ac-grenoble.fr> Hinde, Frank George (Corvallis) a crit : > --> > > > Your right that is exactly what is happening. It also gets worse as > the temperature of the fuel increases, namely thru a hot engine driven > pump...I gets worse further with altitude and the harder you suck on > the fuel. When it gets really bad its called vapour lock and your > engine quits. It will also happen more with autofuel than with 100LL > due to the higher vapour pressure of the mogas. Low wing airplanes > (with wing tanks and no header tank are much more susceptable because > the engine driven pump is sucking uphill. > > This coindiently may happen at the worse possible time i.e a hot > Summer day at a high altitude airport where your fuel has been heat > soaked....You run full power, the engine gets real hot and Here come > the trees! > > So, what to do?....Mount a low pressure electric pump as close to the > outlet of tha tank as possible with no pressure drop on the inlet side > of the pump. > Frank, Thank you for responding. Actually we have wing tanks and our pumps are on the firewall, some inches higher than wing root level. To date we've reached FL 145 in winter on Avgas, and recently flew at FL 135 on Mogas without any problems. I also flew at 37C OAT (only up to 6000 ft). But you're right on the pumps in the wing roots in a perfect circuit. Best regards, Gilles http://contrails.free.fr ________________________________________________________________________________
From: BELTEDAIR(at)aol.com
Date: Mar 16, 2007
Subject: Re: Fuel pump tests
Dear List: I have just gotten in on the tail end of this problem, but we have been working with people to come to a solution. We found the fuel selector valve on low wing planes to be leaking air around the shaft but not leaking fuel. IF it were a high wing with a lot of head pressure fuel would seep out. But on low wing planes fuel does not seep out but air in. We built a manometer to prove the theory. We changed the .06 cent "O"ring around the shaft then put a drop of engine oil to make sure it did not pull in. We experienced engine roughness at high power settings returning to normal at lower power settings. If the aux fuel pump were turned on, it made the condition worse. In early 2006 we went back 5 years in the NTSB files and found 99 instances where the engine quit then would run when it was removed from the wreckage. Fuel injected engines are worse due to the high suction. It equates to putting a hole in a straw and trying to drink. This was found on the "Imperial" type valve. This valve was and is used in most GA and experimetal craft. Jess ************************************** AOL now offers free email to everyone. Find out more about what's free from AOL at http://www.aol.com. ________________________________________________________________________________
Subject: Fuel pump tests
Date: Mar 16, 2007
From: "Hinde, Frank George (Corvallis)" <frank.hinde(at)hp.com>
Excuse my sceptisism but it seems you are now relying on a 25cent O ring... and a single point of failure to boot. Personally i would rather redesign the system to be "hydraulically correct" i.e no sucking anywhere in the system as a fuel leak is a minor problem that has good warning qualities (stink). And air leak has almost no warning qualities until your engine stumbles or quits. Of course if you have big lines and very low pressure drop through the valve on the inlet side to the pump the problem is much reduced on a suck type system, but if you have electric pumps anyway then its worth putting them in the correct place if space permits. As you say, this has resulted in wreckage! Frank ________________________________ From: owner-engines-list-server(at)matronics.com [mailto:owner-engines-list-server(at)matronics.com] On Behalf Of BELTEDAIR(at)aol.com Sent: Friday, March 16, 2007 7:51 AM Subject: Re: Engines-List: Fuel pump tests Dear List: I have just gotten in on the tail end of this problem, but we have been working with people to come to a solution. We found the fuel selector valve on low wing planes to be leaking air around the shaft but not leaking fuel. IF it were a high wing with a lot of head pressure fuel would seep out. But on low wing planes fuel does not seep out but air in. We built a manometer to prove the theory. We changed the .06 cent "O"ring around the shaft then put a drop of engine oil to make sure it did not pull in. We experienced engine roughness at high power settings returning to normal at lower power settings. If the aux fuel pump were turned on, it made the condition worse. In early 2006 we went back 5 years in the NTSB files and found 99 instances where the engine quit then would run when it was removed from the wreckage. Fuel injected engines are worse due to the high suction. It equates to putting a hole in a straw and trying to drink. This was found on the "Imperial" type valve. This valve was and is used in most GA and experimetal craft. Jess ________________________________ AOL now offers free email to everyone. Find out more about what's free from AOL at AOL.com <http://www.aol.com?ncid=AOLAOF00020000000339> . ________________________________________________________________________________
Date: Mar 18, 2007
From: Dan Rogers <drogers(at)maf.org>
Subject: Lycoming Cylinder question
I have some questions about Lycoming Cylinders. I understand that all their 360 and 540 engines use the same size cylinders. Also that there are 2 types of cylinders: Straight valve and Angle valve. I know what the cylinders look like and can easily tell the difference but what are the differences in engine application? How can you know whether a IO540 L (for example, if there is such a thing) has one or the other type of cyl? Do the high HP engines have one type and the Lower hp the other type? Is one type of cylinder newer than the other? Thanks, Dan ________________________________________________________________________________
From: "William Becker" <wbecker(at)centurytel.net>
Subject: Re: Lycoming Cylinder question
Date: Mar 18, 2007
I'm no expert but, The angle valve engines make more HP due to better flow. They are both manufactured currently. Bill B ----- Original Message ----- From: "Dan Rogers" <drogers(at)maf.org> Sent: Sunday, March 18, 2007 12:58 PM Subject: Engines-List: Lycoming Cylinder question > > I have some questions about Lycoming Cylinders. I understand that all > their 360 and 540 engines use the same size cylinders. Also that there > are 2 types of cylinders: Straight valve and Angle valve. I know what the > cylinders look like and can easily tell the difference but what are the > differences in engine application? How can you know whether a IO540 L > (for example, if there is such a thing) has one or the other type of cyl? > Do the high HP engines have one type and the Lower hp the other type? Is > one type of cylinder newer than the other? > > Thanks, > > Dan > > > -- > > ________________________________________________________________________________
From: Gary Casey <glcasey(at)adelphia.net>
Subject: Re: Lycoming Cylinder question
Date: Mar 19, 2007
I'm not "the" Lycoming expert, but as far as I can tell everything with a power rating of 300 or more has the angle-valve cylinders. A sure-fire way to tell is to look at the Lycoming spec sheet on their website and the parallel-valve engines are narrower. Other than that the model numbers don't give much of a clue unless you just know which is which. As Bill said, the angle-valve heads flow better. The naturally-aspirated versions have a 8.7 compression ratio vs. the 8.5 of the parallel-valve engine, and that also helps to produce slightly more power. With more space between the valves the angle- valve engine requires less pressure drop for cooling, theoretically reducing cooling drag. But they are heavier, to the tune of 4 or 5 pounds per cylinder and the angle-valve engines don't have the same reputation for longevity as the parallel-valve engines. An expert told me that there is nothing to be gained by porting and polishing the angle-valve cylinder, while the parallel-valve version can be ported to achieve almost the same airflow as the angle-valve cylinder. Gary Casey Parallel-valve IO-540 with 10:1 compression dyno tested at 305 hp > From: Dan Rogers <drogers(at)maf.org> > Subject: Engines-List: Lycoming Cylinder question > > > I have some questions about Lycoming Cylinders. I understand that all > their 360 and 540 engines use the same size cylinders. Also that > there > are 2 types of cylinders: Straight valve and Angle valve. I know what > the cylinders look like and can easily tell the difference but what > are > the differences in engine application? How can you know whether a > IO540 > L (for example, if there is such a thing) has one or the other type of > cyl? Do the high HP engines have one type and the Lower hp the other > type? Is one type of cylinder newer than the other? > > Thanks, > > Dan ________________________________________________________________________________
Subject: Engine Wanted
Date: Mar 20, 2007
From: <longg(at)pjm.com>
Yes, everyone needs one. I am interested in a Lycoming TIO-360 Turbo or a good rebuilt Continental TSIO-360 Turbo. If Continental, you must provide proof of the crank upgrade. Note, I am looking for a good engine, not a core (unless you want to get rid of it cheap). ________________________________________________________________________________
Date: Mar 20, 2007
From: Dan Rogers <drogers(at)maf.org>
Subject: Re: Lycoming Cylinder question
Thank you, Gary and Bill, I have now studied the Lycoming website engine lists and can see a clear relationship between comp ratio, engine width and weight. There is also power corelation, but because of turbo and various RPM combinations, it is not as clear cut. Thanks again, Dan Gary Casey wrote: > > I'm not "the" Lycoming expert, but as far as I can tell everything with > a power rating of 300 or more has the angle-valve cylinders. A > sure-fire way to tell is to look at the Lycoming spec sheet on their > website and the parallel-valve engines are narrower. Other than that > the model numbers don't give much of a clue unless you just know which > is which. As Bill said, the angle-valve heads flow better. The > naturally-aspirated versions have a 8.7 compression ratio vs. the 8.5 of > the parallel-valve engine, and that also helps to produce slightly more > power. With more space between the valves the angle-valve engine > requires less pressure drop for cooling, theoretically reducing cooling > drag. But they are heavier, to the tune of 4 or 5 pounds per cylinder > and the angle-valve engines don't have the same reputation for longevity > as the parallel-valve engines. An expert told me that there is nothing > to be gained by porting and polishing the angle-valve cylinder, while > the parallel-valve version can be ported to achieve almost the same > airflow as the angle-valve cylinder. > Gary Casey > Parallel-valve IO-540 with 10:1 compression dyno tested at 305 hp > > ________________________________________________________________________________
Date: Mar 20, 2007
From: "Kelly McMullen" <apilot2(at)gmail.com>
Subject: Re: Lycoming Cylinder question


January 19, 2007 - March 21, 2007

Engines-Archive.digest.vol-ap