RotaxEngines-List Digest Archive

Sat 12/11/10


Total Messages Posted: 10



Today's Message Index:
----------------------
 
     1. 04:53 AM - Re: Rotax E-Learning video on detonation and pre-ignition (Matt Tucciarone)
     2. 06:41 AM - Re: Rotax E-Learning video on detonation and pre-ignition (Roger Lee)
     3. 07:36 AM - Oil Info, myths? (Richard Girard)
     4. 08:06 AM - Re: Re: Rotax E-Learning video on detonation and pre-ignition (Noel Loveys)
     5. 09:28 AM - Re: Re: Rotax E-Learning video on detonation and pre-ignition (Matt Tucciarone)
     6. 12:40 PM - Icing: 912S versus 912 (NEEL Jean Philippe)
     7. 03:36 PM - Re: Icing: 912S versus 912 (Rob Housman)
     8. 04:58 PM - Re: Rotax E-Learning video on detonation and pre-ignition (Roger Lee)
     9. 08:27 PM - Re: Re: Rotax E-Learning video on detonation and pre-ignition (Noel Loveys)
    10. 08:57 PM - Re: Rotax E-Learning video on detonation and pre-ignition (Roger Lee)
 
 
 


Message 1


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    Time: 04:53:50 AM PST US
    From: "Matt Tucciarone" <m.tucciarone@hotmail.com>
    Subject: Re: Rotax E-Learning video on detonation and pre-ignition
    ?Thanks for sending the link. I have had the conversation with a friend, that flies an Air Cam, about continuous cruse RPM. He has his engines (912s) at 4500. This video says to keep it above 5200. I cruse at 5300-5500. -----Original Message----- From: Roger Lee Sent: Friday, December 10, 2010 6:10 PM Subject: RotaxEngines-List: Rotax E-Learning video on detonation and pre-ignition FYI Rotax E-Learning video on detonation and pre-ignition. Watch it. http://rotax-owner.com/index.php?option=com_content&view=article&id 1:detonation&catid=15:training&Itemid=174 -------- Roger Lee Tucson, Az. Light Sport Repairman - Maintenance Rated Rotax Repair Center Home 520-574-1080 TRY HOME FIRST Cell 520-349-7056 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=322879#322879


    Message 2


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    Time: 06:41:25 AM PST US
    Subject: Re: Rotax E-Learning video on detonation and pre-ignition
    From: "Roger Lee" <ssadiver1@yahoo.com>
    912's If you only have a ground adjustable prop then we try to balance the climb/cruise setup up and make the engine happy at the same time. The best WOT flat & level rpm is 5500 WOT. This gives you good climb, good cruise speed and the best fuel economy for an individual rpm setting. Balance is the key. This is a good place to be too if you have to fly your plane at WOT because of an emergency like a broken carb cable on one side then you can do that without any problem at 5500 WOT. If you have it set over 5550 then you would be limited to a 5 min. run time. 5500 is Rotax's continuous run rpm. A good cruise rpm (with the max WOT rpm at 5500) is 5000-5300 depending on the plane and application. I prefer and Rotax too, 5100-5300 for cruise. If you run on only 100LL then cruise at 5300 to help keep the lead blown out. At a 5500 WOT rpm then your take off rpms will be up to 5000 or more. This take off rpm will depend now on what flap setting and what climb angle you chose that will either load or help unload the prop. Your planes over all configuration will play a part in this, too. Never set your engine up to only run (i.e. 5000-5200) WOT rpm. It loads the engine too much and over time it will cause problems that you won't see until it's too late. These low rpm settings really overload an engine at take off with rpms below 5000. Having an engine setup to run 5300 or less rpm WOT throttle is counter productive. You get worse climb, worse cruise and worse fuel economy. I have proven this to hundreds of people so there really isn't a valid argument to set your WOT to low cruise rpms. If you have a special need for a better climb prop, like living and flying at very high airports, altitudes or maybe a float fly, ect... then you may need a higher rpm setting to accommodated the special circumstances, plus you will get better performance while flying at the high altitudes with a little flatter pitch. Everyones pitch on the prop setting will be different because we all live and fly at different altitudes, have differen! t props and different fuselage aircraft. I will say that if you truly want to see 5200 on take off as Rotax wants then your WOT flat and level is closer most likely 5700 or more. For me personally this isn't a good balance. having the prop to get 5500 rpm WOT has another big plus. If you screw up a landing and need that full throttle save then the prop/engine rpm spin up is quick and more likely to save your tail. If the rpm was set too low then rpm spin up is slow and it will result in poor save my tail time. All bets are off for the lucky few that have an in flight adjustable prop. They can get the best of all worlds. But even with these guys if they have set the prop to only turn 5100-5200 WOT during cruise then it's counter productive and over loads the engine. Just because they have an in flight adjustable prop doesn't always mean they use it properly. Cruising in the 4000 rpm range for extended periods is not good for your engine. It is ok for a short look at something and landing setups, but not for a constant use. Your engine was specifically designed to run all it's life in the 5000's. It was never intended to run in the 4000's and is really hard on the engine over time and has much more vibration. Be nice to your engine it cost $20K and it is one of the only things keeping you in the air and safe. -------- Roger Lee Tucson, Az. Light Sport Repairman - Maintenance Rated Rotax Repair Center Home 520-574-1080 TRY HOME FIRST Cell 520-349-7056 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=322924#322924


    Message 3


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    Time: 07:36:52 AM PST US
    Subject: Oil Info, myths?
    From: Richard Girard <aslsa.rng@gmail.com>
    There are things that stick in the memory. One that stuck in mine, and I can't remember if it was from Rotax or LSARM classes, was about mixing two stroke oils. Specifically, mixing API rated two cyle oil (API TC) and NMMA TCW-3 would cause them to congeal. Knowing this I stocked up on Pennzoil Air Cooled which is API TC rated so I wouldn't have to worry about draining and cleaning out my 582's rotary valve oiling system. I have always advised other 582 owners to know what oil is used in the rotary valve system, too. Yesterday a customer took delivery of a new to him airplane at my place and the previous owner had sent along a couple of pints of Pennzoil Air Cooled (the 582 has oil injection, too). When I looked at the bottle the first thing I saw was that it is now NMMA TCW-3 rated. Is this compatible with the older oil or not? Rick Girard -- Zulu Delta Kolb Mk IIIC 582 Gray head 4.00 C gearbox 3 blade WD Thanks, Homer GBYM It is not bigotry to be certain we are right; but it is bigotry to be unable to imagine how we might possibly have gone wrong. - G.K. Chesterton


    Message 4


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    Time: 08:06:17 AM PST US
    From: "Noel Loveys" <noelloveys@yahoo.ca>
    Subject: Re: Rotax E-Learning video on detonation and pre-ignition
    What is the best WOT with the tail tied down? Around what pitch angle is a good place to start? (80 hp 912 UL) Noel -----Original Message----- From: owner-rotaxengines-list-server@matronics.com [mailto:owner-rotaxengines-list-server@matronics.com] On Behalf Of Roger Lee Sent: December 11, 2010 11:09 AM Subject: RotaxEngines-List: Re: Rotax E-Learning video on detonation and pre-ignition 912's If you only have a ground adjustable prop then we try to balance the climb/cruise setup up and make the engine happy at the same time. The best WOT flat & level rpm is 5500 WOT. This gives you good climb, good cruise speed and the best fuel economy for an individual rpm setting. Balance is the key. This is a good place to be too if you have to fly your plane at WOT because of an emergency like a broken carb cable on one side then you can do that without any problem at 5500 WOT. If you have it set over 5550 then you would be limited to a 5 min. run time. 5500 is Rotax's continuous run rpm. A good cruise rpm (with the max WOT rpm at 5500) is 5000-5300 depending on the plane and application. I prefer and Rotax too, 5100-5300 for cruise. If you run on only 100LL then cruise at 5300 to help keep the lead blown out. At a 5500 WOT rpm then your take off rpms will be up to 5000 or more. This take off rpm will depend now on what flap setting and what climb angle you chose that will e! ither load or help unload the prop. Your planes over all configuration will play a part in this, too. Never set your engine up to only run (i.e. 5000-5200) WOT rpm. It loads the engine too much and over time it will cause problems that you won't see until it's too late. These low rpm settings really overload an engine at take off with rpms below 5000. Having an engine setup to run 5300 or less rpm WOT throttle is counter productive. You get worse climb, worse cruise and worse fuel economy. I have proven this to hundreds of people so there really isn't a valid argument to set your WOT to low cruise rpms. If you have a special need for a better climb prop, like living and flying at very high airports, altitudes or maybe a float fly, ect... then you may need a higher rpm setting to accommodated the special circumstances, plus you will get better performance while flying at the high altitudes with a little flatter pitch. Everyones pitch on the prop setting will be different bec! ause we all live and fly at different altitudes, have differen! t props and different fuselage aircraft. I will say that if you truly want to see 5200 on take off as Rotax wants then your WOT flat and level is closer most likely 5700 or more. For me personally this isn't a good balance. having the prop to get 5500 rpm WOT has another big plus. If you screw up a landing and need that full throttle save then the prop/engine rpm spin up is quick and more likely to save your tail. If the rpm was set too low then rpm spin up is slow and it will result in poor save my tail time. All bets are off for the lucky few that have an in flight adjustable prop. They can get the best of all worlds. But even with these guys if they have set the prop to only turn 5100-5200 WOT during cruise then it's counter productive and over loads the engine. Just because they have an in flight adjustable prop doesn't always mean they use it properly. Cruising in the 4000 rpm range for extended periods is not good for your engine. It is ok for a short look at something and landing setups, but not for a constant use. Your engine was specifically designed to run all it's life in the 5000's. It was never intended to run in the 4000's and is really hard on the engine over time and has much more vibration. Be nice to your engine it cost $20K and it is one of the only things keeping you in the air and safe. -------- Roger Lee Tucson, Az. Light Sport Repairman - Maintenance Rated Rotax Repair Center Home 520-574-1080 TRY HOME FIRST Cell 520-349-7056 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=322924#322924


    Message 5


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    Time: 09:28:42 AM PST US
    From: "Matt Tucciarone" <m.tucciarone@hotmail.com>
    Subject: Re: Rotax E-Learning video on detonation and pre-ignition
    ?The video says stay above 5200. You say 5100 to 5300. Who is correct? -----Original Message----- From: Roger Lee Sent: Saturday, December 11, 2010 9:38 AM Subject: RotaxEngines-List: Re: Rotax E-Learning video on detonation and pre-ignition 912's If you only have a ground adjustable prop then we try to balance the climb/cruise setup up and make the engine happy at the same time. The best WOT flat & level rpm is 5500 WOT. This gives you good climb, good cruise speed and the best fuel economy for an individual rpm setting. Balance is the key. This is a good place to be too if you have to fly your plane at WOT because of an emergency like a broken carb cable on one side then you can do that without any problem at 5500 WOT. If you have it set over 5550 then you would be limited to a 5 min. run time. 5500 is Rotax's continuous run rpm. A good cruise rpm (with the max WOT rpm at 5500) is 5000-5300 depending on the plane and application. I prefer and Rotax too, 5100-5300 for cruise. If you run on only 100LL then cruise at 5300 to help keep the lead blown out. At a 5500 WOT rpm then your take off rpms will be up to 5000 or more. This take off rpm will depend now on what flap setting and what climb angle you chose that will e! ither load or help unload the prop. Your planes over all configuration will play a part in this, too. Never set your engine up to only run (i.e. 5000-5200) WOT rpm. It loads the engine too much and over time it will cause problems that you won't see until it's too late. These low rpm settings really overload an engine at take off with rpms below 5000. Having an engine setup to run 5300 or less rpm WOT throttle is counter productive. You get worse climb, worse cruise and worse fuel economy. I have proven this to hundreds of people so there really isn't a valid argument to set your WOT to low cruise rpms. If you have a special need for a better climb prop, like living and flying at very high airports, altitudes or maybe a float fly, ect... then you may need a higher rpm setting to accommodated the special circumstances, plus you will get better performance while flying at the high altitudes with a little flatter pitch. Everyones pitch on the prop setting will be different bec! ause we all live and fly at different altitudes, have differen! t props and different fuselage aircraft. I will say that if you truly want to see 5200 on take off as Rotax wants then your WOT flat and level is closer most likely 5700 or more. For me personally this isn't a good balance. having the prop to get 5500 rpm WOT has another big plus. If you screw up a landing and need that full throttle save then the prop/engine rpm spin up is quick and more likely to save your tail. If the rpm was set too low then rpm spin up is slow and it will result in poor save my tail time. All bets are off for the lucky few that have an in flight adjustable prop. They can get the best of all worlds. But even with these guys if they have set the prop to only turn 5100-5200 WOT during cruise then it's counter productive and over loads the engine. Just because they have an in flight adjustable prop doesn't always mean they use it properly. Cruising in the 4000 rpm range for extended periods is not good for your engine. It is ok for a short look at something and landing setups, but not for a constant use. Your engine was specifically designed to run all it's life in the 5000's. It was never intended to run in the 4000's and is really hard on the engine over time and has much more vibration. Be nice to your engine it cost $20K and it is one of the only things keeping you in the air and safe. -------- Roger Lee Tucson, Az. Light Sport Repairman - Maintenance Rated Rotax Repair Center Home 520-574-1080 TRY HOME FIRST Cell 520-349-7056 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=322924#322924


    Message 6


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    Time: 12:40:03 PM PST US
    From: NEEL Jean Philippe <jeanphilippeneel@yahoo.fr>
    Subject: Icing: 912S versus 912
    Hi all,=0AI flown my europa with a 912 80hp during 1200h/11years.It's a mar k one but with =0AXS engine mounting and cowlings.Majority of flights took place here in the =0AFrench Alps as well in -summer as in winter. I never had icing-issue although I =0Ahad no carb preheater-.The only caution I had ,when descending-,was to keep =0A4500/4800 rpm .-Never in idle po sition.=0AIn the beggining of that year I change-my-912-for a new 912 S 100hp. That new =0Aengine has now about 125h. Yesterday I had for the fir st time a rough running =0Aduring few seconds.Outer Air Temp was negative a t every level and the issue =0Aoccurs at the end of a descent 4500/4800rpm from 8000ft to 1500ft. There was =0Aabout- 8=B0C- of difference at grou nd level betwen OAT and dew point.=0ASeveral time I read on Rotax and Europ a web site discussions about icing issues =0Aand I-kept in mind that 912S should be more sensitive to icing than 912.=0A=0AAs-I know:=0A* -Ca rbs are the same ,except needle diam (2.72 versus 2.70 on S)-and ,may be, =0Amain fuel jet-and diffuser (in accordance with needle)-.Does those difference =0Acould explain more-sensitivity to icing?=0A* Compression ratio and bore-are increased on S--but stroke is the same-. In my =0Aopinion these difference have not thing to do with icing issue.=0A-So here is my question-:-Could some body explain why a 912S should be more =0Aexposed to icing than a 912?=0A=0AJean-Philippe Neel=0AF-PSLH Kit N=B02 73=0AGrenoble France-----=0A=0A=0A


    Message 7


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    Time: 03:36:41 PM PST US
    From: "Rob Housman" <rob@hyperion-ef.com>
    Subject: Icing: 912S versus 912
    The cooling (isentropic throttling) that makes carb icing happen is a function of the amount of fuel vaporized so with all other things being equal (same atmospheric conditions, engine manifold, carbs, RPM, etc.) you can expect the somewhat greater fuel flow (more power requires more fuel) to cause more cooling and hence a greater propensity to make ice. Obviously the 912 and 912S are =93different=94 engines but those differences are internal and downstream from the carbs. The 914 is less prone to carb ice because the air compressed by the turbo is warmer than the intake air. Thermodynamics rules! Best regards, Rob Housman Irvine, California Europa XS S/N A070 Rotax 914 Airframe complete Avionics soon From: owner-rotaxengines-list-server@matronics.com [mailto:owner-rotaxengines-list-server@matronics.com] On Behalf Of NEEL Jean Philippe Sent: Saturday, December 11, 2010 12:35 PM Subject: RotaxEngines-List: Icing: 912S versus 912 Hi all, I flown my europa with a 912 80hp during 1200h/11years.It's a mark one but with XS engine mounting and cowlings.Majority of flights took place here in the French Alps as well in summer as in winter. I never had icing issue although I had no carb preheater .The only caution I had ,when descending ,was to keep 4500/4800 rpm . Never in idle position. In the beggining of that year I change my 912 for a new 912S 100hp. That new engine has now about 125h. Yesterday I had for the first time a rough running during few seconds.Outer Air Temp was negative at every level and the issue occurs at the end of a descent 4500/4800rpm from 8000ft to 1500ft. There was about 8=B0C of difference at ground level betwen OAT and dew point. Several time I read on Rotax and Europa web site discussions about icing issues and I kept in mind that 912S should be more sensitive to icing than 912. As I know: * Carbs are the same ,except needle diam (2.72 versus 2.70 on S) and ,may be, main fuel jet and diffuser (in accordance with needle) .Does those difference could explain more sensitivity to icing? * Compression ratio and bore are increased on S but stroke is the same . In my opinion these difference have not thing to do with icing issue. So here is my question : Could some body explain why a 912S should be more exposed to icing than a 912? Jean-Philippe Neel F-PSLH Kit N=B0273 Grenoble France


    Message 8


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    Time: 04:58:17 PM PST US
    Subject: Re: Rotax E-Learning video on detonation and pre-ignition
    From: "Roger Lee" <ssadiver1@yahoo.com>
    Actually both are correct. Rotax publishes numbers like that, but there are way to many applications in the world for everyone to be spot on, so why try to be at least close. Then the teachings in school aren't right along with the book either. So we try to balance a little. Plus we all have different setups. If you are at least 5000+ on take off and at 5500+ WOT you can sleep well at night. Hi Noel, Setting the rpm on the ground static is just to get close. Pitch angle does no good unless you are talking about two identical planes and props. The only way to really tell after that course static adjustment is to get into the air and get some real flight numbers. Shoot for around 5200 static on the ground and that will get you close enough for a flight test to dial it in where it really needs to be. -------- Roger Lee Tucson, Az. Light Sport Repairman - Maintenance Rated Rotax Repair Center Home 520-574-1080 TRY HOME FIRST Cell 520-349-7056 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=322996#322996


    Message 9


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    Time: 08:27:54 PM PST US
    From: "Noel Loveys" <noelloveys@yahoo.ca>
    Subject: Re: Rotax E-Learning video on detonation and pre-ignition
    What would you recommend to be a preliminary AOA for the prop? Warp, nickel edge, square tip, 72" on a Kitfox II? Noel -----Original Message----- From: owner-rotaxengines-list-server@matronics.com [mailto:owner-rotaxengines-list-server@matronics.com] On Behalf Of Roger Lee Sent: December 11, 2010 9:26 PM Subject: RotaxEngines-List: Re: Rotax E-Learning video on detonation and pre-ignition Actually both are correct. Rotax publishes numbers like that, but there are way to many applications in the world for everyone to be spot on, so why try to be at least close. Then the teachings in school aren't right along with the book either. So we try to balance a little. Plus we all have different setups. If you are at least 5000+ on take off and at 5500+ WOT you can sleep well at night. Hi Noel, Setting the rpm on the ground static is just to get close. Pitch angle does no good unless you are talking about two identical planes and props. The only way to really tell after that course static adjustment is to get into the air and get some real flight numbers. Shoot for around 5200 static on the ground and that will get you close enough for a flight test to dial it in where it really needs to be. -------- Roger Lee Tucson, Az. Light Sport Repairman - Maintenance Rated Rotax Repair Center Home 520-574-1080 TRY HOME FIRST Cell 520-349-7056 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=322996#322996


    Message 10


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    Time: 08:57:33 PM PST US
    Subject: Re: Rotax E-Learning video on detonation and pre-ignition
    From: "Roger Lee" <ssadiver1@yahoo.com>
    Hi Noel, If you are flying with floats you may want a little flatter pitch for a little better climb off the water with more weight. I have no recommendation for the pitch, but only to set the static at 5200-5300 and go out and give it a try. I know you have been flying your plane, so what is your WOT setting right now and how does it perform? Just a side note* That particular prop from Warp isn't recommended by Rotax because of it's inertia weight. -------- Roger Lee Tucson, Az. Light Sport Repairman - Maintenance Rated Rotax Repair Center Home 520-574-1080 TRY HOME FIRST Cell 520-349-7056 Read this topic online here: http://forums.matronics.com/viewtopic.php?p=323017#323017




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