Rotax OM-912 Operator's Manual
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Rotax OM-912 Operator's Manual

Rotax OM-912 Operator's Manual

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OPERATORS MANUAL
FOR ROTAX® ENGINE TYPE 912 SERIES
Ref. No.: OM-912
ROTAX ® 912 ULS 3
WITH OPTIONS
part no.: 899374

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  • Page 1 �������� ������� OPERATORS MANUAL FOR ROTAX® ENGINE TYPE 912 SERIES Ref. No.: OM-912 ROTAX ® 912 ULS 3 WITH OPTIONS part no.: 899374...
  • Page 2 Introduction Foreword BRP-Powertrain provides “Instructions for Continued Airworthi- ness”, which are based on the design, the tests and certification of the engine and its components. These instructions apply only to engines and components sup- plied by BRP-Powertrain. This Operators Manual contains important information about safe operation of the engine, together with descriptions of the system and its layout, technical data, operating media and the operational limits of the engine.
  • Page 3 NOTES BRP-Powertrain Effectivity: 912 Series page INTRO-2 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 4 LEP) List of effective pages Chapter Page Date Chapter Page Date cover page 04 01 2010 04 01 2010 INTRO INTRO-1 04 01 2010 04 01 2010 INTRO-2 04 01 2010 04 01 2010 LEP-1 11 01 2010 04 01 2010 LEP-2 04 01 2010 11 01 2010...
  • Page 5 NOTES BRP-Powertrain Effectivity: 912 Series page LEP-2 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 6 TOA) Table of amendments Approval* The technical content of this document is approved under the authority DOA No. EASA.21J.048. current chapter page date of remark for date of approval date of signature change approval from authorities issue 1 to 9 04 01 2010 DOA* LEP-1...
  • Page 7 NOTES BRP-Powertrain Effectivity: 912 Series page TOA-2 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 8 TOA) Summary of changes Content Summary of the relevant amendments in this context, but makes no claim to completeness. current chapter page date of change comment 1 up to 9 04 01 2010 New layout 2-4, 2-7 11 01 2010 Engine start operating temperature description 2-10 11 01 2010...
  • Page 9 NOTES BRP-Powertrain Effectivity: 912 Series page TOA-4 OM Edition 2 / Rev. 1 November 01/2010...

  • Page 10: Table Of Contents

    If any passages of the Manual are not clearly understood or in case of any questions, please, contact an authorized Distributor or Service Center for ROTAX aircraft engines. We wish you much pleasure and satisfaction flying your aircraft with this ROTAX engines.

  • Page 11: General Note

    For additional information on engines, maintenance or parts, you can also contact your nearest authorized ROTAX-aircraft engine distributor (Chapter 9.2). Engine serial num- When making inquiries or ordering parts, always indicate the en- gine serial number, as the manufacturer makes modifications to the engine for product improvement.

  • Page 12: Abbreviations And Terms Used In This Manual

    Kilowatt List of effective pages Newton meter Operators Manual part no. Part number Research Octane Number ROTAX is a trade mark of BRP-Powertrain GmbH & Co KG Revolutions per minute Society of Automotive Engineers Service Instruction Service Bulletin Service Letter...

  • Page 13: Safety

    1.3) Safety General note Although the reading of such information does not eliminate the hazard, understanding the information will promote its correct use. Always use common workshop safety practice. The information and components-/system descriptions contained in this Manual are correct at the time of publication. BRP-Powertrain, however, maintains a policy of continuous im- provement of its products without imposing upon itself any obliga- tion to install them on its products previously manufactured.

  • Page 14: Safety Notice

    WARNING or death! Unless correctly equipped to provide enough electrical power for night VFR (according la- test requirement as ASTM), the ROTAX 912 UL/ULS/ULSFR is restricted to DAY VFR only. Certain areas, altitudes and conditions present greater risk than others. The engine may require humidity or dust/sand preventative equipment, or additional maintenance may be re- quired.
  • Page 15 Instrumentation Select and use proper aircraft instrumentation. This instru- mentation is not included with the ROTAX engine package. Only approved instrumentation may be installed. Engine log book Keep an engine log book and respect engine and aircraft maintenance schedules.
  • Page 16 Engine run Never operate the engine without sufficient quantities of oper- ating fluids (oil, coolant, fuel). Never exceed the maximum permitted operational limits. In the interest of safety, the aircraft must not be left unattended while the engine is running. To eliminate possible injury or damage, ensure any loose equipment or tools are properly secured before starting the en- gine.

  • Page 17: Technical Documentation

    The status of Manuals can be determined by checking the table of amendments of the Manual. The 1 column of this table is the re- vision status. Compare this number to that listed on the ROTAX WebSite: www.rotax-aircraft-engines.com. Updates and current revisions can be downloaded for free. Revision pages...
  • Page 18 Illustrations The illustrations in this Manual are mere sketches and show a ty- pical arrangement. They may not represent the actual part in all its details but depict parts of the same or similar function. There- fore deduction of dimensions or other details from illustrations is not permitted.

  • Page 19: Standard Version

    1.6) Standard version Serial production 4-stroke, 4 cylinder horizontally opposed, spark ignition engi- ne, one central cam-shaft - push-rods - OHV Liquid cooled cylinder heads Ram air cooled cylinders Dry sump forced lubrication Dual breakerless capacitor discharge ignition 2 constant depression carburetors mechanical fuel pump Electric starter (12 V 0.7 kW) Integrated AC generator with external rectifier-regulator (12 V...

  • Page 20: Type Description

    1.7) Type description e.g. 912 A 2 The type designation is of the following composition. ROTAX Description Description Configuration Type: 4-cyl. horizontally opposed, nor- mal aspirated engine Certification: certified to JAR 22 (TC No. EASA.E.121) F, S certified to FAR 33 (TC No.
  • Page 21 1.8) Denomination of cylinders, Engine views, components Lateral view Part Function propeller gear box vacuum pump or hydraulic governor for con- stant speed propeller Fig. 2 00337 Top view Cyl. 1 Cyl. 3 Cyl. 4 Cyl. 2 Part Function engine serial number CD carburetor electric starter expansion tank with excess pressure valve...
  • Page 22 Front view Fig. 4 00336 BRP-Powertrain Effectivity: 912 Series page 1-13 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 23: Technical Data

    1.9) Technical data See table Description 912 A/F/UL 912 S/ULS Bore 79.5 mm (3.13 in) 84 mm (3.31 in) Stroke 61 mm (2.40 in) 61 mm (2.40 in) Displacement 1211 cm (73.9 in 1352 cm (82.5 in Compression ratio. 9.0 : 1 11 : 1 1.10) Fuel consumption See table...
  • Page 24 912 F/S FAR 33 (TC No. E00051 EN), JAR-E (TC No. EASA.E.121). Table of contents This chapter of the Operators Manual contains the operating limits that must be observed to ensure the ROTAX aircraft engine and standard systems operate safely. Subject Page...

  • Page 25: Operating Limits (912 A/F/Ul)

    2.1) Operating limits (912 A/F/UL) Performance data relate to ISA (International Standard Atmo- Performance sphere) conditions without Governor, external alternator etc. Take-off performance 59.6 kW at 5800 rpm Max. continuous performance 58 kW at 5500 rpm Speed Take-off speed 5800 rpm (max. 5 min) Max.

  • Page 26: Conventional Coolant

    Conventional See also Chapter 2.3). coolant Coolant temperature: (coolant exit temperature) Max. 120 °C (248 °F) Cylinder head temperature: Max. 150 °C (300 °F) Permanent monitoring of coolant temperature and cylinder head temper- ature is necessary. Waterless coolant See also Chapter 2.3).

  • Page 27: Fuel Pressure

    Engine start, oper- ating temperature Max. 50 °C (120 °F) (ambient temperature) Min. -25 °C (-13 °F) (oil temperature) Fuel pressure Non-compliance can result in serious injuries WARNU WARNING or death! Exceeding the max. admissible fuel pressure will override the float valve of the carburetor and to engine failure.

  • Page 28: Operating Limits (912 S/Uls)

    2.2) Operating limits (912 S/ULS) Performance data relate to ISA (International Standard Atmo- Performance sphere) conditions without Governor, external alternator etc. Take-off performance 73.5 kW at 5800 rpm Max. continuous performance 69 kW at 5500 rpm Speed Take-off speed 5800 rpm (max. 5 min) Max.

  • Page 29: Conventional Coolant

    Conventional See also Chapter 2.3). coolant Coolant temperature: (coolant exit temperature) Max. 120 °C (248 °F) Cylinder head temperature: Max. 135 °C (275 °F) Permanent monitoring of coolant temperature and cylinder head temper- ature is necessary. Waterless coolant Cylinder head temperature: Max.

  • Page 30: Fuel Pressure

    Engine start, oper- ating temperature Max. 50 °C (120 °F) (ambient temperature) Min. -25 °C (-13 °F) (oil temperature) Fuel pressure Non-compliance can result in serious injuries WARNU WARNING or death! Exceeding the max. admissible fuel pressure will override the float valve of the carburetor and to engine failure.

  • Page 31: Coolant

    2.3) Operating media-Coolant General note Obey the latest edition of Service Instruction NOTICE WARNUNG SI-912-016 for the selection of the correct coolant. Conventional Conventional coolant mixed with water has the advantage of a coolant higher specific thermal capacity than water-less coolant. Application When correctly applied, there is sufficient protection against vapor bubble formation, freezing or thickening of the coolant within the...
  • Page 32 2.4) Operating media-Fuel General note Obey the local codes and the latest edition of NOTICE WARNUNG Service Instruction SI-912-016 for the selec- tion of the correct fuel. Use only fuel suitable for the respective cli- NOTICE WARNUNG matic zone. NOTE: Risk of vapour formation if using winter fuel for summer operation.
  • Page 33 2.5) Operating media-Lubricants General note Obey the manufacturers instructions about NOTICE WARNUNG the lubricants. If the engine is mainly run on AVGAS more frequent oil changes will be required. See Service Information SI-912-016, latest edi- tion. Motorcycle oil of a registered brand with gear additives. Do Oil type not use aircraft engine oil for direct driven engines.
  • Page 34 Table of lubricants See Fig. 1 Since the temperature range of neighboring SAE grades overlap, there is no need for change of oil viscosity at short duration of am- bient temperature fluctuations. Klima Mehrbereichs-Öle °C °F (climatic multi-grade oils conditions) tropisch (tropical) gemäßigt...
  • Page 35 NOTES BRP-Powertrain Effectivity: 912 Series page 2-12 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 36 3) Standard operation Introduction To warrant reliability and efficiency of the engine, meet and care- fully observe all the operating and maintenance instructions. Table of content This chapter of the Operators Manual contains expanded operat- ing and maintenance instructions. Subject Page Daily checks page 3-2...
  • Page 37 3.1) Daily checks General note To warrant reliability and efficiency of the engine, meet and care- fully observe all the operating and maintenance instructions. Risk of burnings and scalds! WARNU WARNING Hot engine parts! Conduct checks on the cold engine only! Non-compliance can result in serious injuries WARNU WARNING...
  • Page 38 Coolant level The coolant specifications of the section NOTICE WARNUNG Operating media are to be ob- Chapter 2.3) served! Step Procedure Verify coolant level in the expansion tank, replenish as re- quired up to top. The max. coolant level must be filled up to the top (see Fig.
  • Page 39 Check of mechanical components Check of mech. components Step Procedure Turn propeller by hand in direction of engine rotation sev- eral times and observe engine for odd noises or excessive resistance and normal compression. At excessive resistance of the engine per- NOTICE WARNUNG form the relevant unscheduled maintenance...
  • Page 40 3.2) Before engine start Carry out pre-flight checks. 3.3) Pre-flight checks Safety Non-compliance can result in serious injuries WARNU WARNING or death! Ignition “OFF”. Before moving the propeller. Switch off both ignition circuits and anchor the aircraft. Have the cockpit occupied by a competent person.
  • Page 41 The oil specifications of the section Chapter NOTICE WARNUNG Operating media are to be observed! 2.5) Step Procedure Check oil level and replenish as required. NOTE: Propeller shouldn't be turned exces- sively reverse the normal direction of engine rotation. Remove oil tank cap. Prior to oil check, turn the propeller by hand in direction of engine rotation several times to pump oil from the engine into the oil tank.
  • Page 42 3.4) Engine start Safety Non-compliance can result in serious injuries WARNU WARNING or death! Do not take the engine into operation if any person is near the aircraft. Engine start Step Designation Procedure Fuel valve open Starting carb activated Then engine in operating tempera- start the engine without ture...
  • Page 43 Reduction gear with shock absorber To observe! Since the engine comprises a reduction gear NOTICE WARNUNG with shock absorber, take special care of the following: Step Procedure To prevent impact load, start with throttle lever in idle position or at the most up to 10% open. For the same reason, wait for around 3 sec.
  • Page 44 3.5) Prior to take-off Safety Non-compliance can result in serious injuries WARNU WARNING or death! Do not take the engine into operation if any person is near the aircraft. Warming up peri- Step Procedure Start warming up period at approx. 2000 rpm for approx. 2 minutes.
  • Page 45 3.6) Take-off Safety Non-compliance can result in serious injuries WARNU WARNING or death! Monitor oil temperature, cylinder head temperature and oil pressure. Limits must not be exceeded! See Oper- Chapter 2.1) ating limits. Respect “cold weather operation” recommendations, see Chapter 3.9). Climb Climbing with engine running at take-off performance is permissi- ble (max.
  • Page 46 3.9) Cold weather operation General note Generally, an engine service should be carried out before the start of the cold season. Coolant For selection of coolant and mixing ratio, see "Coolant", Chapter 2.3) Lubricant For selection of oil, see table of Lubricants Chapter 2.5) Cold start With throttle closed and choke activated (open throttle renders...
  • Page 47 Icing due to water in fuel Icing due to water in fuel Fuels containing alcohol always carry a small NOTICE WARNUNG amount of water in solution. In case of tem- perature changes or increase of alcohol con- tent, water or a mixture of alcohol and water may settle and could cause troubles.
  • Page 48 4) Abnormal operation Introduction Non-compliance can result in serious injuries WARNU WARNING or death! At unusual engine behaviour conduct checks as per Maintenance Manual, Chapter 05-50- 00 before the next flight. NOTE: Further checks - see Maintenance Manual. Table of contents This chapter of the Operators Manual contains expanded operat- ing and maintenance instruction at abnormal operation.

  • Page 49: Start During Flight

    4.1) Start during flight Engine stop Starting procedure same as on ground, however, on a warm engine without choke. 4.2) Exceeding of max. admissible engine speed Exceeding of max. Reduce engine speed. Any exceeding of the max. admissible engine speed engine speed has to be entered by the pilot into the logbook, stating the duration and extend of overspeed.

  • Page 50: Oil Pressure Below Minimum - During Flight

    4.5) Oil pressure below minimum - during flight Oil pressure below minimum Reduce engine power setting to the minimum NOTICE WARNUNG necessary and carry out precautionary land- ing. Check oil system. 4.6) Oil pressure below minimum - on ground Immediately stop the engine and check for reason. Check oil sys- tem.

  • Page 51: Trouble Shooting

    4.7) Trouble shooting Introduction All checks in accordance with the Maintenance Manual (current issue/revision). Non-compliance can result in serious injuries WARNU WARNING or death! Only qualified staff (authorized by the Avia- tion Authorities) trained on this particular en- gine, is allowed to carry out maintenance and repair work.

  • Page 52: Knocking Under Load

    Engine does not start Starting problems Possible cause Remedy Ignition off. switch on. Closed fuel valve or clogged open valve, clean or renew filter, check filter. fuel system for leaks. No fuel in tank. refuel. Starting speed too low, faulty fit fully charged battery.
  • Page 53 Oil level is increasing Oil level Possible cause Remedy Oil too cold during engine op- cover oil cooler surface, maintain the oil eration. temperature prescribed. Engine hard to start at low temperature Cold engine start Possible cause Remedy Starting speed too low. preheat engine.
  • Page 54 5) Performance data Introduction The performance tables and performance graphs on the next few pages are intended to show you what kind of performance to ex- pect from your engine in terms of power output. The indicated power can be achieved by following the procedures laid out in the Operators Manual and ensuring that the engine is well-main- tained.
  • Page 55 Performance graphs for stand. conditions (ISA) Performance graphs Engine 912 A/F/UL 3000 4000 5000 5800 rpm A: max. engine output B: power requirement of propeller Fig. 1 00450 (Gal/h) in.Hg (7,93) (5,28) (2,64) 3000 4000 5000 5800 rpm C: manifold pressure D: fuel consumption Values along propeller curve Fig.
  • Page 56 Performance data for variable pitch propeller Performance data Engine 912 A/F/UL Engine speed over 5500 rpm is restricted to 5 minutes. Run the engine in accordance with the following table. Engine Perfor- Manifold Torque (Nm) Power setting speed mance pressure (ft.lb) (rpm) (kW)/(HP)
  • Page 57 Performance data variable pitch propeller Performance data Engine 912 A/F/UL The following graph shows the performance drop with increasing flight altitude. The curves show the performance at 5800, 5500, 5000, 4500 and 4000 rpm, at full throttle. The engine allows operation with fully open throttle valve over the whole rpm range, without limitation.

  • Page 58: Brp-Powertrain

    Performance Performance graphs for stand. conditions (ISA) graphs Engine 912 S/ULS Fig. 4 02001 Ansaugladedruck manifold pressure Werte bezogen auf die Propeller-Kurve values along propeller curve Benzinverbrauch fuel consumption 5800 2500 3000 3500 4000 4500 5000 5500 Drehzahl/Engine speed [1/min / rpm] Fig.
  • Page 59 Performance data for variable pitch propeller Performance data Engine 912 S/ULS Engine speed over 5500 rpm is restricted to 5 minutes. Run the engine in accordance with the following table. Engine Perfor- Manifold Power set- Torque (Nm) speed mance pressure ting (ft.lb) (rpm)
  • Page 60 Performance Performance graph for non-standard conditions graph The following graph shows the performance drop with increasing Engine 912 S/ULS flight altitude. The curves show the performance at 5800, 5500, 5000, 4800 and 4300 rpm, at full throttle. The engine allows operation with fully open throttle valve over the whole rpm range, without limitation.
  • Page 61 NOTES BRP-Powertrain Effectivity: 912 Series page 5-8 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 62 6) Weights Introduction The stated weights are dry weights (without operating fluids) and are guide values only. Further weight information relating to the equipment can be found in the current Installation Manual. Table of content This chapter of the Operators Manual contains an extensive list of approved equipment for this engine.
  • Page 63 6.1) Engine with: electric starter, carburetors, internal generator, ignition unit and oil tank without: exhaust system, radiator, airbox Configuration 2 912 UL 912 A 912 F 912 ULS 912 S 57.1 kg (126 lb) 58.3 kg (128 lb) with overload with overload 57.1 kg 57.1 kg...
  • Page 64 7) Description of systems Introduction This chapter of the Operator Manual contains the description of cooling system, fuel system, lubrication system, electric system and the propeller gearbox. Table of content As already mentioned in the preface, the system descriptions only apply to the engine, not to a specific application in a particular air- craft.
  • Page 65 See Fig. 1. Cooling The cooling system of the ROTAX 912 is designed for liquid coo- ling of the cylinder heads and ram-air cooling of the cylinders. The cooling system of the cylinder heads is a closed circuit with an ex- pansion tank.
  • Page 66 Cooling system Part Function expansion tank radiator pressure cap overflow bottle Fig. 1 09152 BRP-Powertrain Effectivity: 912 Series page 7-3 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 67 7.2) Fuel system General note See Fig. 2 Fuel The fuel flows from the tank (1) via a coarse filter (2) the fire cock (3) and fine filter (4) to the mechanical fuel pump (5). From the pump fuel passes on via the fuel manifold (6) to the two carbure- tors.
  • Page 68 7.3) Lubrication system General note See Fig. 3 The ROTAX 912 engine is provided with a dry sump forced lubri- cation system with a main oil pump with integrated pressure regu- lator (1) and oil pressure sensor (2). Lubrication The oil pump (3) sucks the motor oil from the oil tank (4) via the oil cooler (5) and forces it through the oil filter (6) to the points of lu- brication in the engine.
  • Page 69 Oil system Part Function pressure regulator oil pressure sensor oil pump oil tank oil cooler oil filter venting tube oil temperature sensor Fig. 3 08650 BRP-Powertrain Effectivity: 912 Series page 7-6 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 70 7.4) Electric system General note See Fig. 4 The ROTAX 912 engine is equipped with a dual ignition unit of a breakerless, capacitor discharge design, with an integrated gene- rator. The ignition unit needs no external power supply. Charging coils Two independent charging coils (1) located on the generator sta- tor supply one ignition circuit each.
  • Page 71 7.5) Propeller gearbox General note See Fig. 5 Reduction ratio For the engine type 912 two reduction ratios are available. Reduction ratio 912 A/F/UL 912 S/ULS crankshaft: propeller shaft 2.27:1 2.43:1 2.43:1 (optional) Overload clutch Depending on engine type, certification and configuration the pro- peller gearbox is supplied with or without an overload clutch.
  • Page 72 Backlash On the gearbox version with overload clutch the design incorpo- rates a friction damped free play at the dogs to warrant proper en- gine idling. Due to this backlash at the dogs a distinct torsional impact arises at start, stop and at sudden load changes, but due to the built-in overload clutch it will remain harmless.
  • Page 73 NOTES BRP-Powertrain Effectivity: 912 Series page 7-10 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 74 8) Checks Introduction All checks to be carried out as specified in the current Mainte- nance Manual (last revision). Non-compliance can result in serious WARNU WARNING injuries or death! Only qualified staff (authorized by the Avi- ation Authorities) trained on this particu- lar engine, is allowed to carry out maintenance and repair work.
  • Page 75 Due to the special material of the cylinder wall, there is no need for extra protection against corrosion for the ROTAX aircraft engi- nes. At extreme climatic conditions and for long out of service pe-...
  • Page 76 In case of any relevant occurrences that may involve mal- function of the engine, the form on the next page should be filled out and sent to the responsible authorized ROTAX distributor. ®...
  • Page 77 NOTES BRP-Powertrain Effectivity: 912 Series page 9-2 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 78 9.1) Form BRP-Powertrain Effectivity: 912 Series page 9-3 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 79 NOTES BRP-Powertrain Effectivity: 912 Series page 9-4 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 80 9.2) Authorized Distributor General note See the official ROTAX AIRCRAFT ENGINES Homepage ® www.rotax-aircraft-engines.com List Overview of authorized distributor for ROTAX aircraft engines. Subject Page page 9-6 Europe page 9-7 America Australia page 9-7 Africa page 9-7 page 9-8 Asia...
  • Page 81 1) E U R O P E Issue 2010 11 01 CROATIA / FORMER YUGOSLAVIA GREAT BRITAIN / IRELAND / (EXEPT SLOVENIA): ICELAND: ➤SHAFT D.O.O. ➤SKYDRIVE LTD. B.L. Mandica 161 a Burnside, Deppers Bridge HR-54000 OSIJEK SOUTHAM, WARWICKSHIRE CV47 2SU Tel.: +385 (0) 31 /280-046, Tel.: +44 (0) 1926 / 612 188, Fax: +385 (0) 31 /281-602...
  • Page 82 2) A M E R I C A NORTH / MIDDLE / SOUTH AMERICA: CANADA: ➤KODIAK RESEARCH LTD. P.O. Box N 658 ➤ROTECH RESEARCH CANADA, LTD. Bay & Deveaux Street 6235 Okanagan Landing Rd. NASSAU, BAHAMAS VERNON, B.C., V1H 1M5, CANADA Tel.: +1 242 / 356 5377, Tel.: +1 250 / 260-6299, Fax: +1 242 / 356 2409...
  • Page 83 5) A S I A ISRAEL: CHINA / HONG KONG / MACAO: ➤CONDOR-AVIATION INDUSTRIES LTD. P.O. Box 1903, 14 Topaz st. ➤PEIPORT INDUSTRIES LTD. Cesaria 38900 Rm. 1302, Westlands Centre Tel.: +972 (0) 4 / 6265080, 20 Westlands Road, Quarry Bay Fax: +972 (0) 4 / 6265095 HONG KONG E-mail: condor@netvision.net.il...
  • Page 84 Motornummer / Engine serial no. Flugzeugtype / Type of aircraft Flugzeugkennzeichen / Aircraft registration no. ROTAX® Vertriebspartner ROTAX® authorized distributor www.rotax-aircraft-engines.com ® and TM are trademarks of BRP-Powertrain GmbH & Co KG. © 2010 BRP-Powertrain GmbH & Co KG. All rights reserved.

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