SERVICE INSTRUCTION
Contents
1. types 912 914 is designed for operation with waterless coolant and thus must not be modified i e drainage or ventilation holes must not be closed NOTE With waterless coolant based on propylene glycol such as EVANS NPG it is sufficient to monitor the cylinder head temperature since the boiling point is very high CAUTION Thecertification and determination of the correct coolant type must be conducted by the aircraft manufacturer As each aircraft type has different characteristics testing must be done to determine the most suitable coolant and instrumentation for each aircraft type Recommended coolant 100 concentrate Marke brand Bezeichnung description EVANS NPG EVANS _ NPGR ee CAUTION EVANS NPGR contraction point is approx 23 C 10 F It will not freeze and expand like conventional coolant Do not use if conditions expose the engine to non operational temperatures below 23 C 10 F 4 3 1 Warnings for operating with waterless coolant Water or coolant containing water must never be added to the cooling system The max water content must not exceed 3 6 it can be tested using a Brix refractometer Any water present in the cooling system is separated out as vapor This can cause the cooling system to fail due to insufficient coolant quantity If EVANS NPG NPGR is not available locally for servicing the cooling system a conventional coolant based on ethylene glycol can be2. used temporarily However the coolant must be replaced again with EVANS NPG NPGR within the next 15 days M CAUTION As some conventional coolants are available in a pre mixed formula water added be sure you only add 100 pure ethylene glycol if EVANS NPG NPGR is not available E CAUTION The above warnings are taken from the manufacturer s user manual however the original text and description in the user manual is binding APRIL 07 2008 SI 912 016 R1 SI 914 019 R1 Copyright ROTAX page 7 of 10 5 Fuel 5 1 General Different requirements such as air purity laws led to the development of fuel types with different compositions such as fuel enriched with oxygen Development is focused more on better and cleaner combustion and less on the effects on the engine equipment and power The main focus is environmental protection The problem is in the variety and changeability of the types of fuel currently available for sale and the damaging effects of some types of fuel Thus it is necessary for the aircraft operator to check with each batch of gasoline that the fuel is suitable for the engine Buy fuel only from large well known brands and dealers that openly declare the actual octane number Do everything to get confirmation that the purchased fuel corresponds to the fuel declared at the fueling point Obtain technical base data on the fuel used such as octane number addition of ethanol methanol as oxygen carrier Seas
3. 04286 ROTAX AIRCRAFT ENGINES SERVICE INSTRUCTION SELECTION OF SUITABLE OPERATING FLUIDS FOR ROTAX ENGINE TYPE 912 AND 914 SERIES SI 912 016 R1 SI 914 019 R1 Repeating symbols Please pay attention to the following symbols throughout this document emphasizing particular information AWARNING Identifies an instruction which if not followed may cause serious injury or even death MCAUTION Denotes an instruction which if not followed may severely damage the engine or could lead to suspension of warranty NOTE Information useful for better handling 1 Planning information 1 1 Engines affected All versions of the engine type 912 Series 914 Series 1 2 Concurrent ASB SB SI and SL In addition to this Service Instruction the following additional Service Bulletin must be observed and complied with SB 912 043 SB 914 29 Change of coolant specification current issue 1 3 Reason Field experience has shown that additional information about the choice of suitable operating fluids such as motor oil coolant and fuel and about oil change and maintenance intervals for ROTAX engine types 912 and 914 is necessary 1 4 Subject Selection of suitable operating fluids for ROTAX engine type 912 and 914 Series Thisinformation should help the aircraft builder and operator ensure that the operating conditions and installation are correct and thereby achieve optimum performance and reliability 1 5 Com
4. AS 91 96 UL 91 96 UL 5 HJELMCO AVGAS HJELMCO AVGAS 91 98 UL 91 98 UL 3 eB a DS a Anti Knock Index RON MON 2 min RON 90 min RON 95 min AKI 87 min AKI 91 unleaded available most important in Scandinavian area 09102 AVGAS 100LL places greater stress on the valve seats due to its high lead content and forms increased deposits in the combustion chamber and lead sediments in the oil system Thus it should only be used in case of problems with vapor lock or when other types of gasoline are unavailable CAUTION Use only the correct fuel for the specific climate zones HINWEIS There is a risk of vapor lock formation if winter fuel is used for summer operation APRIL 07 2008 Copyright ROTAX SI 912 016 R1 SI 914 019 R1 page 9 of 10 6 General engine operation requirements and operating tips Keep the motor oil temperature below 120 C 250 F over most of the operating period Always insure that the oil type used is adequate for climatic conditions and peak engine operating temperatures If operational oil temperatures exceed 120 C 250 F use of a mineral or petroleum based oil is not recommended For turbocharged engines ensure an adequate running cool down period to prevent deposits by coking of oil When operating with unleaded fuels or MOGAS and when engine oil temperatures often exceed 120 C 250 F use of a high quality full synthetic oil is recommended To avoi
5. Loss of octane rating is a common problem on fuel stored incorrectly which could lead directly to engine damage or stoppage Current FAA guidelines require that auto fuel approved for aircraft Mogas meet stricter guidelines than that of regular car gas This may be the simplest way to maintain some control over what you are using even so scrutinize carefully Alcohol ethanol will attract and retain water this water can freeze in cold conditions and from the carburation action the water lowers the vaporization point of fuel and could cause vapour lock the water may not be detectable in your fuel system Alcohol is a solvent which could clean deposits in your fuel system and carry them into the filters or carburetors Alcohol burns leaner and may cause higher exhaust gas temperatures EGTs 07830 APRIL 07 2008 SI 912 016 R1 SI 914 019 R1 Copyright ROTAX page 8 of 10 5 1 2 Fuel according to local standards The following fuels can be used Usage Description 912 UL A F 912 ULS S 914 UL F MOGAS n EN 228 Normal uropean P EN 228 Super EN 228 Super standard EN 228 Super plus EN 228 Super plus Canadian CAN CGSB 3 5 i standard Quality 1 3 CAN CGSB 3 5 Quality 3 US standard ASTM D4814 ASTM D4814 AVGAS AVGAS 100 LL AVGAS 100 LL US standard ASTM D910 ASTM D910 released brand name HJELMCO AVGAS HJELMCO AVG
6. additives such as good quality 4 stroke motorcycle oils are highly recommended Because of the incorporated friction clutch oils with friction modifier additives are unsuitable because this could result in clutch slipping during standard operation Heavy duty semi or fully synthetic depending on fuel type used brand name oils offer many advantages and are generally the best choice Avoid oils designed strictly for use in Diesel engines These may not be suitable due to insufficient high temperature properties and additives that may affect the operation of the slipper clutch in the gear box Incase of severe operating conditions i e flight school towing near idle operation over a long period over use of carburetor preheating etc the time between maintenance intervals must be generally shorter and in particular the frequency of oil changes must be increased regardless of the type of fuel mainly used MOGAS or AVGAS On turbocharged engines always conduct a cool down run before shutting down in accordance with the relevant Operators Manual Careful attention to engine operation tips see section 6 APRIL 07 2008 SI 912 016 R1 SI 914 019 R1 page 2 of 10 Copyright ROTAX 3 2 Operation with unleaded and low lead fuel less than 0 1 g liter lead content When operating primarily on unleaded fuels or MOGAS the maintenance intervals remain unchanged from the published maintenance schedule found in the currently val
7. after every 50 operating hours change of oil filter change of engine oil oil level checks etc according to the most recent Maintenance Manual In addition compliance with the following operating conditions is required HM CAUTION The engine is considered to be operated mainly on leaded AVGAS when run for more than 30 of engine operating time on leaded AVGAS fuel NOTE When operating primarily on leaded AVGAS fuel we recommend to make a change of engine oil every 25 operating hours More frequent oil changes will assure timely removal of residues and oil sludge thus avoiding increased wear or operating troubles Use the following oils and observe the oil specification indicated Motor oils recommended for use with leaded AVGAS Marke i PEE Spezifikation Viskosit t Code brand Bezeichnung description specification viscosity code SHELL AeroShell Sport Plus 4 API SL SAE 10 W 40 2 SHELL Advance VSX 4 API SG SAE 10 W 40 3 SHELL Formula Shell Synthetic Blend API SL SAE 10 W 30 4 SHELL Formula Shell API SJ SAE 10 W 30 5 SHELL Formula Shell API SJ SAE 20 W 50 5 Valvoline DuraBlend Synthetic API SJ SAE 10 W 40 4 MOBIL Mobil 1 Clean 7500 API SM SL SAE 10 W 30 4 Evva EVVA Mehrbereichs l C52 multigrade oil C52 APISJ CF SAE 15 W 50 3 08421 1 recommendation code 2 Semi synthetic aviation oils with gear additives Highly recommended for n
8. d formation of condensation water in the motor oil the oil temperature must rise at least once every operational day to at least 100 C 212 F When safe and sensible avoid extended use of carburetor air pre heating The type of fuel used operating conditions and the demands of the engine mission profile may need to increase the frequency of oil changes to avoid the excessive build up of lead and other residues in the engine oil Always adjust the engine oil change intervals to avoid excessive build up of sludge in the engine oil MCAUTION Donotuse oil additives and observe the operating limits as per the relevant Operator s Manual Excessive engine vibration particularly at low idle speeds can impair the carburetor fuel metering system leading to atoo rich mixture condition This rich mixture condition can further lead to rough engine operation and excessive carbon and lead deposits Observance of the following maintenance and operating tips can reduce engine vibration and maintain accurate carburetor fuel metering Regular pneumatic synchronization of the carburetors and synchronization of bowden cable for throttle and choke adjustment can greatly improve the smoothness of engine operation Proper adjustment of the engine idle speed and maintenance of the air induction system can also aid smooth engine operation and helps to maintain the correct air fuel mixture Proper air fuel mixture will reduce the separation of the non volatil
9. e components in leaded AVGAS and helps to minimize the rate of lead deposition in the engine Whenever safe and sensible the engine should be operated at speeds between 2500 and 2750 crankshaft RPM 1100 to 1200 propeller RPM with 2 27 1 reduction ratio 1050 to 1150 propeller RPM with 2 43 1 reduction ratio after starting and during the initial warm up period Avoid rapid changes in engine RPM immediately after start up Rapid engine cooling down resulting from altitude changes performed at a low power setting landing approaches flown at low power settings or rapid engine shut down after landing or ground operations should be avoided Maintain engine speed between 2500 and 2750 crankshaft RPM 1100 to 1200 propeller RPM with 2 27 1 reduction ratio 1050 to 1150 propeller RPM with 2 43 1 reduction ratio until engine temperatures have stabilized before stopping the engine Maintaining high friction torque values on the gear reduction unit can reduce vibrations from the torsion load absorber further reducing overall engine vibrations particularly at low RPM Correct balancing of the propeller to a tolerated value can greatly reduce engine vibration decrease wear of engine and gear reduction unit components improve engine performance and add to engine life Recent developments in electronic propeller balancing equipment now allow quick dynamic balancing of propellers without removing the propeller from the aircraft Other benefits of correct propell
10. er balance include the reduction of cockpit noise and vibration levels and a reduction in fatigue of exhaust components air boxes sheet metal components cowlings engine linkages and aircraft sections Regular compliance with SI 912 005 SI 914 007 Lubrication System for all ROTAX Engine Types 912 series and 914 series current version will assure proper function of the engine lubrication system and optimum engine life 7 Summary A WARNING Non compliance with these recommendations could result in engine damage personal injury or death Approval of translation to best knowledge and judgment in any case the original text in the German language and the metric units Sl system are authoritative APRIL 07 2008 SI 912 016 R1 Copyright ROTAX SI 914 019 R1 page 10 of 10
11. hly recommended for normal lower than 120 C 250 F and high oil temperature higher than 120 C 248 F operation using leaded or unleaded fuels 3 Semi synthetic motorcycle oils with gear additives Highly recommended for normal lower than 120 C 250 F and high oil temperature higher than 120 C 248 F operation using leaded or unleaded fuels 4 Semi synthetic oil Recommended for normal lower than 120 C 248 F and high oil temperature higher than 120 C 250 F operation using leaded or unleaded fuels 5 Full synthetic oil Recommended for high oil temperature operation higher than 120 C 248 F using only unleaded fuels The viscosity column is only a guideline Substituting other than that shown is acceptable Example Formula Shell Synthetic Blend SAE 5W 30 is a substitute for 10W 30 The guidelines given here must however be obeyed in all cases using only those oils with which there have already been good operating experiences on ROTAX engine types 912 and 914 series NOTE The coefficient of viscosity indicates the tendency of oil to flow but it is not necessarily a quality code Country specific deviations of the viscosity are possible APRIL 07 2008 Copyright ROTAX SI 912 016 R1 SI 914 019 R1 page 3 of 10 3 3 Operation with leaded AVGAS fuels If the engine is mainly operated with leaded AVGAS fuels the following maintenance operations are necessary in addition by latest
12. id Maintenance E CAUTION Manual for the engine type In case of severe operating conditions the time between maintenance intervals must be generally shorter and in particular the frequency of oil changes must be increased regardless of the type of fuel mainly used MOGAS or AVGAS Use the following oils and observe the oil specification indicated Motor oils recommended for use with unleaded fuel or MOGAS 08420 Marke RER Spezifikation Viskosit t Code Bezeichnung description e i brand specification viscosity code SHELL AeroShell Sport Plus 4 API SL SAE 10 W 40 2 SHELL Advance VSX 4 API SG SAE 10 W 40 3 SHELL Advance VSX 4 API SG SAE 15 W 50 3 SHELL Advance Ultra 4 API SJ SAE 10 W 40 1 SHELL Formula Shell Synthetic Blend API SL SAE 10 W 30 4 MOBIL Mobil 1 API SJ CF SAE 5 W 30 5 MOBIL Mobil 1 API SJ CF_ SAE 15 W 50 5 MOBIL Mobil 1 MX4T APISG CF _ SAE 10 W 40 1 MOBIL Mobil 1 V Twin API SG CF SAE 20W 50 1 MOBIL Mobil 1 Clean 7500 APISM SL SAE 10W 30 4 Yacco MVX 500 Synthetic API SJ SAE 10 W 40 3 EVVA EVVA Mehrbereichs l C52 multigrade oil C52 API SJ CF SAE 15 W 50 3 1 recommendation code 1 Full synthetic motorcycle oil with gear additives Highly recommended for high oil temperature operation higher than 120 C 250 F using only unleaded fuels 2 Semi synthetic aviation oils with gear additives Hig
13. l mixture can cause water and fuel contamination in the oil reducing its lubrication capacity Furthermore long down times with oil that contains water and contaminants can cause corrosion damage especially on the bearings with serious consequential damage The criteria for correct motor oil selection are Correct oil viscosity for cold starts and sufficient oil pressure at high temperatures Good gear wear protection Avoidance of clutch slipping due to incorrect additives Insufficient oil flow capability so that too much volume remains in the engine leading to low oil level in the external oil tank This can only be detected during testing with an oil level indicator installed on the oil tank Ability to withstand combustion products containing lead which enter the oil during AVGAS operation High oil temperature durability This is especially important for the turbo engine due to the risk of oil carbon build up on the bearing and sealing seats of the turbocharger The oil carbon build up coking can also flake off and block restrict the oil return passage Conclusions f possible operate the listed engine types using unleaded or low lead fuel AVAGS 100 LL is not considered low leaded in this context Use the recommended motor oils according to sections 3 2 and 3 3 of this Service Instruction Use only oil with API classification SG or higher Due to high stresses in the reduction gears oils with gear
14. ngine types 912 914 and careful selection is advised following the recommendations in this Service Instruction NOTE In principle ROTAX has not approved any specific oils but oils must meet certain quality requirements ROTAX only recommends the oils described in Sections 3 2 and 3 3 of this Service Instruction ROTAX is aware of formulation changes to some oils previously recommended for use in this Service Instruction As a result ROTAX no longer recommends following oils and these should not be used anymore sneer Bezeichnung description ia Castrol Castrol Power 1 API SJ Castrol GPS API SG CD MOTUL 5100 Synthetic Blend API SJ APRIL 07 2008 SI 912 016 R1 SI 914 019 R1 Copyright ROTAX page 5 of 10 4 Coolant 4 1 General All engine types 912 914 have liquid cooled cylinder heads and ram air cooled cylinders The function of the coolant is to protect the cylinder heads from over temperature by means of heat dissipation Protection against corrosion of the engine components and freezing of the coolant is achieved with appropriate additives In principle 2 different types of coolant are permitted Conventional coolant based on ethylene glycol with 50 water content Waterless coolant based on propylene glycol 4 2 Conventional coolant Conventional coolant with about 50 water content has a specific thermal capacity that is higher than waterless coolant It gives excellent co
15. onal additives etc In general oxygen carriers alcohol additives are to be avoided Fuel with more than 5 alcohol added must not be used Checking the fuel for alcohol content is the only sure way to ensure that your fuel is suitable for your ROTAX engine CAUTION The ill effects of alcohol in your engine are as follows The alcohol will attract water this can cause your sediment traps e g in the fuel tank to flood plug filters and restrict fuel flow Also and very important the alcohol competes directly with the lubrication and depending on your oils ability to combat such could cause engine damage Important also is the alcohol carries water which on engine shut down and storage can create corrosion on vital engine parts such as crank main and rod bearings as well as pins Once corrosion pittings has started the bearings will fail shortly after Seasonal blend crossovers can affect your fuels volatility if you use a winter blend fuel during a hot summer day This is a common occurrence with people who buy a fuel blend in colder climates in March but don t use it in their ROTAX until June Evaporation temperatures of your fuel must be low enough to minimize crankcase and combustion chamber deposits as well as spark plug fouling without fear of vapour locking or boiling Always make sure you buy your fuel from a high volume user and avoid fuel which has been in storage for long periods of time especially between seasons
16. ormal lower than 120 C 248 F and high oil temperature higher than 120 C 248 F operation using leaded or unleaded fuels 3 Semi synthetic motorcycle oils with gear additives Highly recommended for normal lower than 120 C 248 F and high oil temperature higher than 120 C 248 F operation using leaded or unleaded fuels 4 Semi synthetic oil Recommended for normal lower than 120 C 248 F and high oil temperature higher than 120 C 248 F operation using leaded or unleaded fuels 5 Petroleum based oil Recommended for use only when oil temperatures remain below 120 C 248 F and when using leaded fuels The viscosity column is only a guideline Substituting other than that shown is acceptable providing all temperature limitations are respected Example Formula Shell Synthetic Blend SAE 5W 30 is a substitute for 10W 30 The guidelines given here must however be obeyed in all cases using only those oils with which there have already been good operating experiences on ROTAX engine types 912 and 914 series NOTE The coefficient of viscosity indicates the tendency of oil to flow but it is not necessarily a quality code Country specific deviations of the viscosity are possible APRIL 07 2008 SI 912 016 R1 SI 914 019 R1 Copyright ROTAX page 4 of 10 3 4 Motor oils not suitable for engine types 912 914 Series Experience has shown that only some oils are suitable for use in ROTAX e
17. pliance According Maintenance Manual of engine type ROTAX 912 and 914 Series current issue AWARNING Non compliance with these instructions could result in engine damages personal injuries or death 1 6 Approval The technical content is approved under the authority of DOA Nr EASA 21J 048 1 7 References In addition to this technical information refer to current issue of Operators Manual OM Maintenance Manual MM Installation Manual IM APRIL 07 2008 Current valid documentation see SI 912 016 R1 www rotax aircraft engines com SI 914 019 R1 page 1 of 10 Copyright ROTAX 2 Material Information 2 1 Material cost and availability None 3 Lubricant 3 1 General Foreign particles formed during combustion are suspended in the motor oil Together with oil components that are not sufficiently resistant to heat these foreign particles can cause parts such as pistons piston rings exhaust valves etc to seize and lead to problems On turbocharged engines failing to ensure an adequate cool down period prior to shut off may lead to particle deposits and cause damage to bearings and seals Hard oil residues can obstruct parts of the oil system and lead to damage In addition to insufficient cool down periods the use of unsuitable oils and not obeying oil change intervals can especially cause such damage Long term operation with an engine that is too cold and operating too long with an overly rich fue
18. rrosion protection especially for aluminum and protection against freezing NOTE For exact monitoring of the coolant temperature a limit has been set This is necessary because standard coolant based on ethylene glycol such as BASF Glysantin in a 50 50 proportion mixture can boil at a temperature as low as 120 C 248 F Refer to the current Installation Manual for more information and instructions CAUTION Thecertification and determination of the correct coolant type must be conducted by the aircraft manufacturer As each aircraft type has different characteristics testing must be done to determine the most suitable coolant and instrumentation for each aircraft type Recommended coolant with a mixture of 50 antifreeze and 50 water Marke brand Bezeichnung description BASF Glysantin Protect Plus G48 CASTROL Antifreeze All Climate CASTROL Antifreeze Anti Boil YACCO LR 35 SHELL VELVANA FRIDEX G48 TEXACO Havoline Extended Life Antifreeze Coolant DEX COOL PETROL Antifreeze Concentrate Antifreeze G 11 07180 APRIL 07 2008 S1 912 016 Ri SI 914 019 R1 Copyright ROTAX page 6 of 10 4 3 Waterless coolant Waterless coolant has advantages to prevent boiling of the cooling system because of its high boiling point However the specific thermal capacity is lower than with conventional coolant resulting in slightly higher running temperatures The cooling system of ROTAX engine
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