Rotax 914 Series Operator's Manual
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Rotax 914 Series Operator's Manual

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See also: Maintenance Manual , Installation Manual
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OPERATORS MANUAL
FOR ROTAX® ENGINE TYPE 914 SERIES
Ref. No.: OM-914
ROTAX ® 914 UL 3
WITH OPTIONS
part no.: 899645

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Terry
February 7, 2025

where to disconnect wiring so that the ignition modules are not energized by the internal generator when the engine is rotated? I do not want to touch the pickup coils because that would change the timing.

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1 comments:
Mr. Anderson
February 11, 2025

To prevent the ignition modules from being energized by the internal generator when the engine is rotated on a Rotax 914 Series, disconnect the wiring from the charging coils. The charging coils supply energy to the ignition modules, so removing their connection will prevent the capacitors in the electronic modules from storing energy and firing the ignition system.

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Summary of Contents for Rotax 914 Series

  • Page 1 �������� ������� OPERATORS MANUAL FOR ROTAX® ENGINE TYPE 914 SERIES Ref. No.: OM-914 ROTAX ® 914 UL 3 WITH OPTIONS part no.: 899645...
  • Page 2 This legend shall be included on any reproduction of these data, in whole or in part. The Manual must remain with the engine/aircraft in case of sale. Copyright 2010 © - all rights reserved. ROTAX is a trade mark of BRP-Powertrain GmbH&Co KG. In the following document the ®...
  • Page 3 Chapter 3) Standard operation Chapter 4) Abnormal operation Chapter 5) Performance data Chapter 6) Weights Chapter 7) Description of systems Chapter 8) Checks Chapter 9) Supplements Effectivity: 914 Series BRP-Powertrain page INTRO-1 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 4 NOTES Effectivity: 914 Series BRP-Powertrain page INTRO-2 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 5 04 01 2011 04 01 2010 3-10 04 01 2010 rear page 3-11 04 01 2010 3-12 04 01 2010 3-13 04 01 2010 3-14 04 01 2010 Effectivity: 914 Series BRP-Powertrain page LEP-1 OM Edition 2 / Rev. 1 April 01/2011...
  • Page 6 NOTES Effectivity: 914 Series BRP-Powertrain page LEP-2 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 7 DOA* 04 01 2011 DOA* 04 01 2011 DOA* 4-10 04 01 2011 DOA* 04 01 2011 DOA* 04 01 2011 DOA* 04 01 2011 DOA* Effectivity: 914 Series BRP-Powertrain page TOA-1 OM Edition 2 / Rev. 1 April 01/2011...
  • Page 8 NOTES Effectivity: 914 Series BRP-Powertrain page TOA-2 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 9 04 01 2010 New layout 04 01 2011 Engine start operating temperature description 04 01 2011 Operating fluids - definition 9-6,7,8 04 01 2011 Overview of authorized distributor Effectivity: 914 Series BRP-Powertrain page TOA-3 OM Edition 2 / Rev. 1 April 01/2011...
  • Page 10 NOTES Effectivity: 914 Series BRP-Powertrain page TOA-4 OM Edition 2 / Rev. 1 April 01/2011...

  • Page 11: Table Of Contents

    If any passages of the Manual are not clearly understood or in case of any questions, please, contact an authorized Distribution- or Service Center for ROTAX aircraft engines. We wish you much pleasure and satisfaction flying your aircraft with this ROTAX engines.
  • Page 12 For additional information on engines, maintenance or parts, you can also contact your nearest authorized ROTAX-aircraft engine distributor (Chapter 9.2). When making inquiries or ordering parts, always indicate the en-...
  • Page 13 BRP-Powertrain GmbH & Co KG Revolutions per minute Society of Automotive Engineers Service Instruction Service Bulletin Service Letter Type certificate Table of amendments Visual Flight Rules Effectivity: 914 Series BRP-Powertrain page 1-3 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 14 A revision bar outside of the page margin in- dicates a change to text or graphic. Effectivity: 914 Series BRP-Powertrain page 1-4 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 15 Unless correctly equipped to provide enough electrical power for night VFR (according la- test requirement as ASTM), the ROTAX 914 UL 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 16 Select and use proper aircraft instrumentation. This instru- Instrumentation mentation is not included with the ROTAX engine package. Only approved instrumentation may be installed. Keep an engine log book and respect engine and aircraft Engine log book maintenance schedules.
  • Page 17 This engine may be equipped with a vacuum pump. The safety Vacuum pump warning accompanying the vacuum pump must be given to the owner/operator of the aircraft into which the vacuum pump is installed. Effectivity: 914 Series BRP-Powertrain page 1-7 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 18: Technical Documentation

    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. Further the Manual is in such a way developed that revision pages...
  • Page 19 The illustrations in this Operators Manual are stored in a graphic data file and are provided with a consecutive irrelevant number. This number (e.g. 00277) is of no significance for the content. Effectivity: 914 Series BRP-Powertrain page 1-9 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 20: Standard Version

    External alternator (12 V 40 A DC) Vacuum pump: (only for configuration 2 and 4 possible) Hydraulic constant speed propeller governor: (for configurati- on 3 only) Effectivity: 914 Series BRP-Powertrain page 1-10 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 21: Type Description

    Prop flange for fixed pitch propeller and prepared for retrofit of a hy- draulic governor for constant speed propeller. Effectivity: 914 Series BRP-Powertrain page 1-11 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 22: Denomination Of Cylinders, Engine Views

    Cyl. 2 Cyl. 4 Part Function engine serial number CD carburetor electric starter intake air distributor “Airbox“ fuel pressure control expansion tank with excess pressure valve Effectivity: 914 Series BRP-Powertrain page 1-12 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 23 Part Function turbocharger exhaust system external generator Fig. 3 03645 Front view Fig. 4 03646 Effectivity: 914 Series BRP-Powertrain page 1-13 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 24: Technical Data

    Direction of rotation on propeller shaft: counter clockwise, looking Direction of rota- tion on propeller at p.t.o side of engine. shaft normal direction of propeller rotation (engine) Fig. 5 08629 Effectivity: 914 Series BRP-Powertrain page 1-14 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 25 914 F FAR 33 (TC No. E00058NE),  JAR-E (TC No. EASA.E.122). This chapter of the Operators Manual contains the operating limits Table of contents that must be observed to ensure the ROTAX aircraft engine and standard systems operate safely. Subject Page...

  • Page 26: Operating Limits

    1200 hPa (35.4 in.HG) Limit of engine operation at zero gravity and in negative ”g” con- Acceleration dition. Max. 5 seconds at max. -0.5 g Effectivity: 914 Series BRP-Powertrain page 2-2 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 27: Critical Flying Altitude

    Oil temperature Min. 50 °C (120 °F) normal operating temperature approx. 90 to 110 °C (190 - 230 °F) exhaust gas temperature Max. 950 °C (1742 °F) Effectivity: 914 Series BRP-Powertrain page 2-3 OM Edition 2 / Rev. 1 April 01/2011...

  • Page 28: Conventional Coolant

    Max. Airbox pressure + 0.35 bar (5.08 psi) Min. Airbox pressure + 0.15 bar (2.18 psi) Normal Airbox pressure + 0.25 bar (3.63 psi) Effectivity: 914 Series BRP-Powertrain page 2-4 OM Edition 2 / Rev. 1 April 01/2011...

  • Page 29: Power Consumption Of The Hydraulic Propeller

    1200 W Deviation from bank angle: Bank angle Max. 40° NOTE: Up to this value the dry sump lubrication system warrants lubrication in every flight situation. Effectivity: 914 Series BRP-Powertrain page 2-5 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 30: Operating Media-Coolant

    % designation concentrate water conventional e.g. BASF Glysantine  anticorrosion waterless e.g. EVANS NPG+ * coolant component can be increased up to max. 65 %. Effectivity: 914 Series BRP-Powertrain page 2-6 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 31: Operating Media-Fuel

    Usage/Description AVGAS 914 F/UL Aviation  AVGAS 100 LL Standard (ASTM D910) Effectivity: 914 Series BRP-Powertrain page 2-7 OM Edition 2 / Rev. 1 April 01/2011...

  • Page 32: Operating Media-Lubricants

    They are suitable for use throughout the sea- sons, ensure rapid lubrication of all engine com- ponents at cold start and get less fluid at higher temperatures. Effectivity: 914 Series BRP-Powertrain page 2-8 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 33: Table Of Lubricants

    Klima Mehrbereichs-Öle °C °F (climatic multi-grade oils conditions) tropisch (tropical) gemäßigt (temperate) arktisch (arctic) Fig. 1 01176 Effectivity: 914 Series BRP-Powertrain page 2-9 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 34 NOTES Effectivity: 914 Series BRP-Powertrain page 2-10 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 35 Coolant page 3-12 Lubricant page 3-12 Cold start page 3-12 Icing in the air intake system page 3-12 Icing due to water in fuel page 3-13 Effectivity: 914 Series BRP-Powertrain page 3-1 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 36: Daily Checks

    Mainte- nance Manual is necessary. Do not release the engine into service before rectification. Effectivity: 914 Series BRP-Powertrain page 3-2 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 37: Coolant Level

    Verify coolant level in the overflow bottle, replenish as re- quired. The coolant level must be between max. and min. mark. Expansion tank Graphic Part Function radiator cap expansion tank Fig. 1 08523 Effectivity: 914 Series BRP-Powertrain page 3-3 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 38: Check Of Mechanical Components

    Verify free movement of throttle cable and starting carbu- retor over the complete range. Check from the cockpit. Exhaust system and turbocharger Step Procedure Inspect for damages, leakage and general condition. Effectivity: 914 Series BRP-Powertrain page 3-4 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 39: Before Engine Start

    Step Procedure Verify coolant level in the overflow bottle, replenish as re- quired up to top. The coolant level must be between min. and max. mark. Effectivity: 914 Series BRP-Powertrain page 3-5 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 40: Oil

    Avoid oil levels exceeding the “max“ mark, since excess oil could be poured out through the venting system. Difference between max.- and min.- mark = 0.45 litre (0.95 liq pt) Effectivity: 914 Series BRP-Powertrain page 3-6 OM Edition 2 / Rev. 0...

  • Page 41: Engine Start

    NOTICE (without interruption), followed by a cooling period of 2 minutes! As soon as engine runs adjust throttle to achieve smooth running at approx. 2500 r.p.m. Effectivity: 914 Series BRP-Powertrain page 3-7 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 42 For checking the two ignition circuits, only one circuit may be switched off and on at a time. Effectivity: 914 Series BRP-Powertrain page 3-8 OM Edition 2 / Rev. 0...

  • Page 43: Prior To Take-Off

    Check control of the hydraulic propeller governor to specifications of the manufacturer. NOTE: Cycling the propeller governor puts a relatively high load on the engine. Unnecessary cycling or additional checks should be avoided. Effectivity: 914 Series BRP-Powertrain page 3-9 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 44: Take-Off

    Switch on the auxiliary fuel pump at take-off. Move throttle lever to 115 % (take-off performance). The auxiliary fuel pump should be switched off after the take-off. Effectivity: 914 Series BRP-Powertrain page 3-10 OM Edition 2 / Rev. 0 April 01/2010...

  • Page 45: Take-Off

    NOTICE WARNUNG recorded by the TCU. At exceeding of the lim- its of operation will render any claims on  ROTAX null and void. Step Procedure Switch on the auxiliary fuel pump. Move throttle lever to 115 % (take-off performance).

  • Page 46: Cold Weather Operation

    Manual supplied by the aircraft manufacturer. The turbocharger will heat up the intake air. If however a in- take air pre-heating is necessary, observe the aircraft manu- facturers engine installation and operating instruction. Effectivity: 914 Series BRP-Powertrain page 3-12 OM Edition 2 / Rev. 0...

  • Page 47: Icing Due To Water In Fuel

    Use non-contaminated fuel (filtered through suede) Remedy Generously sized water separators Fuel lines routing inclined Prevent condensation of humidity, i. e avoid temperature dif- ferences between aircraft and fuel. Effectivity: 914 Series BRP-Powertrain page 3-13 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 48 NOTES Effectivity: 914 Series BRP-Powertrain page 3-14 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 49 Oil pressure below minimum - during flight page 4-6 Oil pressure below minimum - on ground page 4-7 Engine on fire or fire in the engine compartment page 4-8 Trouble shooting Effectivity: 914 Series BRP-Powertrain page 4-1 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 50 - full may be fully closed and control of the throttle! boost pressure and rpm is only pos- sible via ignition unit. Effectivity: 914 Series BRP-Powertrain page 4-2 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 51 Pressure control is not possible. Limited flying operation. Switch off servo motor for a moment (max. 5 sec). After a short regulating time opera- tion should stabilize. Effectivity: 914 Series BRP-Powertrain page 4-3 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 52 The boost pressure will not be reduced auto- NOTICE WARNUNG matically. Possible cause Remedy The maximum “take-off“ time lim- Reduce speed and boost pressure at itation was exceeded. least to maximum continuous speed. Effectivity: 914 Series BRP-Powertrain page 4-4 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 53 Reduce engine speed. Any exceeding of the max. admissible Exceeding of max. engine speed engine speed has to be entered by the pilot into the logbook, stating duration and extent of overspeed. Effectivity: 914 Series BRP-Powertrain page 4-5 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 54 Immediately stop the engine and check for reason. Check oil sys- Oil pressure below minimum tem. Check oil quantity in oil tank. Check oil quality. See Chapter 2.4). Effectivity: 914 Series BRP-Powertrain page 4-6 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 55 Any shut-off of the fuel system for short periods or permanent has to be entered by the pilot into the logbook starting date and dura- tion of shut-off. Effectivity: 914 Series BRP-Powertrain page 4-7 OM Edition 2 / Rev. 0...
  • Page 56 Page Starting problems page 4-9 Engine run page 4-9 Oil pressure page 4-9 Oil level page 4-10 Engine hard to start at low temperature page 4-10 Effectivity: 914 Series BRP-Powertrain page 4-8 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 57 Low oil pressure Oil pressure Possible cause Remedy Not enough oil in oil tank. Check oil return line for free passage, renew oil seal. Effectivity: 914 Series BRP-Powertrain page 4-9 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 58 Oil pressure must be measured at idle at an oil NOTE: temperature of minimum 50 °C (120 °F). Be sure the oil pressure does not go below minimum at idle. Effectivity: 914 Series BRP-Powertrain page 4-10 OM Edition 2 / Rev. 1 April 01/2011...
  • Page 59 Subject Page Performance graphs for standard conditions page 5-2 Performance data for variable pitch propeller page 5-4 Performance graph for non-standard conditions page 5-5 Effectivity: 914 Series BRP-Powertrain page 5-1 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 60 *914 F starting with engine no. 4,420.200 (TCU part no. 966741) *914 UL starting with engine no. 4,417.598  (TCU part no. 966471) Fig. 2 08642 Effectivity: 914 Series BRP-Powertrain page 5-2 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 61 Fuel consumption A: Engine curve (take-off performance) B: Engine curve (continuous full throttle performance) C: Propeller curve (Power requirement of propeller) Fig. 3 08643 Effectivity: 914 Series BRP-Powertrain page 5-3 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 62 75 % 5000 55.1 105 77 ft.lb approx. 67 65 % 4800 47.8 70 ft.lb approx. 64 55 % 4300 40.4 66 ft.lb approx. 59 Effectivity: 914 Series BRP-Powertrain page 5-4 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 63 Temperature ISA at 10 000 ft ........ -5 °C Ambient temperature at 10 000 ft ......-15 °C Temperature difference to ISA ......-10 °C Max. continuous power as per table....72 kW Effectivity: 914 Series BRP-Powertrain page 5-5 OM Edition 2 / Rev. 0...
  • Page 64 NOTES Effectivity: 914 Series BRP-Powertrain page 5-6 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 65 This chapter of the Operators Manual contains an extensive list of Table of content approved equipment for this engine. Subject Page page 6-2 Engine page 6-2 Accessories Effectivity: 914 Series BRP-Powertrain page 6-1 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 66 Overload clutch 1.7 kg (3.7 lb) NOTE: The overload clutch is installed on all certified aircraft engines and on non-certified aircraft engines of the configuration 3. Effectivity: 914 Series BRP-Powertrain page 6-2 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 67 Red boost lamp page 7-12 Propeller gearbox page 7-12 Reduction ratio page 7-12 Overload clutch page 7-12 Torsional shock absorber page 7-13 Backlash page 7-13 Vacuum pump Effectivity: 914 Series BRP-Powertrain page 7-1 OM Edition 2 / Rev. 0 April 01/2009...

  • Page 68: Cooling System Of Engine

    7.1) Cooling system of the engine See Fig. 1. General note The cooling system of the ROTAX 914 is designed for liquid coo- Cooling 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 69 Cooling system Part Function expansion tank radiator pressure cap overflow bottle Fig. 1 09152 Effectivity: 914 Series BRP-Powertrain page 7-3 OM Edition 2 / Rev. 0 April 01/2009...

  • Page 70: Fuel System

    Pay attention to possible constriction of diameter or obstruction, to avoid overflow- ing of carburetors. Via the return line (7) surplus fuel flows back to the fuel tank. Effectivity: 914 Series BRP-Powertrain page 7-4 OM Edition 2 / Rev. 0...
  • Page 71 Fuel system MAIN Part Function fuel tank filter/water trap electric fuel pumps fuel pressure control carburetor check valve return line airbox Fig. 2 00103 Effectivity: 914 Series BRP-Powertrain page 7-5 OM Edition 2 / Rev. 0 April 01/2009...

  • Page 72: Lubrication System

    7.3) Lubrication system See Fig. 3 General note The ROTAX 914 engine is provided with a dry sump forced lubri- cation system with a main oil pump with integrated pressure regu- lator (1) and an additional suction pump. The main oil pump (2) sucks the motor oil from the oil tank (3) via...
  • Page 73 (main oil pump) oil line (secondary oil pump to oil tank) oil temperature sensor Fig. 3 08580 Effectivity: 914 Series BRP-Powertrain page 7-7 OM Edition 2 / Rev. 0 April 01/2009...

  • Page 74: Electric System

    7.4) Electric system See Fig. 4 General note The ROTAX 914 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. Two independent charging coils (1) located on the generator sta- Charging coils tor supply one ignition circuit each.

  • Page 75: Turbocharger And Control System

    7.5) Turbo charger and control system The ROTAX 914 engine is equipped with an exhaust gas turbo- General note charger, making use of the energy in the exhaust gas for precom- pression of the intake air (boost pressure). The boost pressure in the airbox is controlled by means of an elec-...

  • Page 76: Nominal Boost Pressure

    ~ 0 % 1500 hPa (44.3 in.HG) max. continuous per- 100-108 % 1220 hPa (36.0 in.HG) formance take-off performance 110-115 % 1370 hPa (40.5 in.HG) Effectivity: 914 Series BRP-Powertrain page 7-10 OM Edition 2 / Rev. 0 April 01/2009...

  • Page 77: Nominal Pressure

    The TCU registers the time of full throttle operation (boost pressure). Full throttle operation for longer than 5 minutes will make the red boost lamp blink. Chapter 4.1) Abnormal operation. Effectivity: 914 Series BRP-Powertrain page 7-11 OM Edition 2 / Rev. 0 April 01/2009...

  • Page 78: Propeller Gearbox

    The design incorporates a torsional shock absorber. The shock Torsional shock absorber absorbing is based on progressive torsional cushioning due to axi- al spring load acting on a dog hub. Effectivity: 914 Series BRP-Powertrain page 7-12 OM Edition 2 / Rev. 0 April 01/2009...

  • Page 79: Backlash

    Transmission ratio between crankshaft and hy- draulic governor or vacuum pump is 1.842 i.e. the speed of the hydraulic governor or vacuum pump is 0.54 of engine speed. Effectivity: 914 Series BRP-Powertrain page 7-13 OM Edition 2 / Rev. 0...
  • Page 80 NOTES Effectivity: 914 Series BRP-Powertrain page 7-14 OM Edition 2 / Rev. 0 April 01/2009...
  • Page 81 8) Checks All checks to be carried out as specified in the current Mainte- Introduction nance Manual (last revision). Non-compliance can result in serious WARNING WARNU 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 82 8.1) Engine preservation Risk of burnings and scalds! General note WARNING WARNU Hot engine parts! Always allow engine to cool down to ambient temperature before start of any work. Due to the special material of the cylinder wall, there is no need for extra protection against internal cylinder corrosion for the RO- TAX aircraft engines.
  • Page 83 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 84 NOTES Effectivity: 914 Serie BRP-Powertrain page 9-2 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 85 9.1) Form Effectivity: 914 Serie BRP-Powertrain page 9-3 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 86 NOTES Effectivity: 914 Serie BRP-Powertrain page 9-4 OM Edition 2 / Rev. 0 April 01/2010...
  • Page 87 9.2) Authorized Distributor AIRCRAFT ENGINES Homepage  See the official ROTAX General note ® www.rotax-aircraft-engines.com Overview of authorized distributors of ROTAX aircraft engines. List Subject Page page 9-6 Europe page 9-7 America Australia page 9-7 Africa page 9-7 page 9-8...
  • Page 88 1) E U R O P E Issue 2011 04 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 89 2) A M E R I C A NORTH / MIDDLE / SOUTH AMERICA: ➤KODIAK RESEARCH LTD. CANADA: 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 90 5) A S I A ISRAEL: ➤LUCIANO SORLINI S.P.A. CHINA / HONG KONG / MACAO: Piazza Roma, 1 ➤PEIPORT INDUSTRIES LTD. Carzago di Calvagese Riviera (Brescia),  Rm. 1302, Westlands Centre Italy 20 Westlands Road, Quarry Bay Tel.: +39 030 / 601 033, HONG KONG Fax: +39 030 / 601 463 Tel.: +852 (0) 2885 / 9525,...
  • Page 92 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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