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I ssoire Aviation / APM Simba / Rotax 915 iS, 915 iSc Rotax aircraft engines, the company and its ownership

BRP is a world leader in the As the largest producer of small design, manufacturing, dis- aircraft engines in the world, tribution, and ma rketing of our aircraft engines are the first choice motorized recreational of more than 250 aircraft manufacturers vehicle s and powersports around the globe. Join us. engines. With our high-performance engines that power the world of mo- tor sports we set the pace for the industry with legendary products such as Ski-Doo and Lynx , Sea-Doo watercraft, Can-Am all-terrain and side-by-side vehicles, and Can-Am Spyder roadsters. Name: Bombardier Recreational Products Inc. (BRP) Headquarters: Valcourt, Québec (Canada) Manufacturing sites: Canada, USA, Mexico, Finland, Employees: 8,700 worldwide Ownership: Shares are traded on the Toronto Stock Exchange under the symbol „DOO“

BRP-rotax is a market leader in the developing and manufacturing of innovative powertrains for powersport products.

Our high-tech premium engines for maximum performance, light weight, fuel efficiency, longevity and reliability, form the hearts of le- gendary BRP products as well as of motorcycles, karts and light and ultralight aircraft. We have developed more than 350 Rotax engine models and produced over 7 million engines.

Nam: e B enefit from improved fuel efficiency, BRP-Rotax GmbH & Co KG low-operating costs, class leading power Locations: Gunskirchen, Austria (Europe) to weight ratio, best in-class useful load Manufacturing sites: and flight range, and the well known Austria, Mexico reliability. Employees: 1,150 Procurement office: Unleash the power, Hong Kong enjoy the lightness, Ownership: 100% subsidiary of BRP exceed your expectations. Rotax aircraft engines, the company and its ownership the Sky is the limit Se pr ad your wings

facts & Figures Icon / A5 / iS Sport

180,000+ Rotax aircraft 60+ Million flying hours engines produced of the rotax 912/914/915 engines fleet 50,000+ engines of the approx. 5 Million flying hours 912/914 engine series produced of the rotax 912/914/915 engines fleet per year 50.000+ rotax aircraft engines in operation our warranties and service network

Wherever you are, we are with you We are committed to highest customer satisfaction by offering you outstanding service and support. The sales and service of our aircraft engines and genuine replacement parts are provided by authorized distributors and their network on all 5 continents in more than 100 countries. Our distributor network has factory trained mechanics and provides professional service for your engine throughout its life. Our service partners have a well-stocked inventory to enable you to spend even more time in the air. Rotax genuine spare parts are covered by the manufacturer’s warranty. Parts availability for Rotax aircraft engines is guaranteed for at least ten years.

Regular warranty for 4- engines 24 months or 400 hours (whatever comes first) of regular warranty for certified 4-stroke engines 18 months or 200 hours (whatever comes first) of regular warranty for non-certified 4-stroke engines

Rotax extended service terms (R.E.S.T.)* Beside the regular manufacturer warranty, the high quality standards enable BRP-Rotax to offer you a special program called the Rotax Ex- tended Service Terms (R.E.S.T.) with two different types of extended warranty for Rotax 4-stroke aircraft engines (this offer only applies if allowed under applicable law).

O ne year plus coverage R.E.S.T. Rotax Extended Service Terms +1 additional year or up to 200 hours, whatever comes first

F ull TBO coverage R.E.S.T. Rotax Extended Service Terms +3 additional years or up to TBO of 2,000 hours, whatever comes first

ENGINE REgistRATION Easy paperless engine registration process Increase of service quality Security feature: no way of re-registration of stolen engines

Service Center

Repair Center

Distributor * only applies to the Rotax 912 and 914 engine series our warranties and service network Worldwide on site At your Service

Service Center In the scope of providing highest quality, our globally standardized attendees from engine operators to maintenance personnel. To offer you Repair Center training program called ”iRMT“ (independent Rotax Maintenance Trai- our full support, manuals, catalogues and all useful documentation are ning) provides the relevant knowledge and technical education to all downloadable free of charge at www.flyrotax.com Distributor the technical details of our exceptional aircraft engines Open yourself to new possibilities

Durability & reliability TREDUNDAN IGNITION SYSTEM DLiquid AN AIR COOLED ET STing PRocedureS EXCEEDING CERTIFICATION STANDARDS

P OWER & PERFORMANCE REDUCTION GEAR BOX SEA E OF USE ADditionAL ALTERNATOR i S Injection Technology

AIR-Fuel MIxture low operating & The iS technology offers optimized air-fuel mixture at all operating conditions as well as easy starts under cold weather conditions operational costs compared to engines. AEUS G OF DIFFERENT FUEL TYPES PErforMANce* Due to a system which is capable for high pressure ratios and to the new designed gearbox with improved gear ratio, sufficient OVERLOAD CLUTCH performance at low rpm is provided to power even 4-seater aircraft consistently up to 15,000 ft with full power.

* Rotax 915 iS/iSc the technical details of our exceptional aircraft engines Open yourself to new possibilities

TRedundAN INJECTORS SEA E OF USE is controlled individually by the ECU via two redundant Various features such as knock control or engine management system injectors per cylinder. This gives you a more fuel-efficient flight thanks (EMS) in combination with other advantages such as no carburator icing to an optimized calibration of the fuel-air mixture. The outcome: longer and transient engine behaviour lead to an improved and easy operation. flight distances. EMS ECO MOde The Engine Management System (EMS) controls ignition, fuel- and air The engines automatically improve its fuel efficiency by switching to a mixture electronically and is implemented redundantly to ensure a higher lean ECO mode once the throttle is pulled back to a throttle setting below level of safety. The system is designed to be single fault redundant. 97% after start and climb phases. ECU DBU S The Electronic Control Unit (ECU) controls the fuel and air mixture The BRP Utility and Diagnostic Software for Rotax aircraft engines electronically and is implemented redundantly into the EMS to ensure (BUDS Aircraft) is designed to give you insight into the engine manage- a higher level of safety. ment system and enables mechanics to make fast engine checks. ROTAx engineS 65 HP 582 UL 80 HP 912 UL/A/F 100 HP 912 ULS/S 100 HP 912 iS/iSc SPORT 115 H P 914 UL/F 141 HP 915 iS/iSc

Over 30,000 units of this popular Rotax 2-stroke engine have been The Rotax 912 series is well regarded for its reliability and efficiency In comparison to the 80 hp version of the Rotax 912 series the 100 The Rotax 912 iS Sport engine offers all well known advantages The turbo charged series offers more performance at Based on the proven concept of the Rotax 912 / 914 engine sold. This engine type is well regarded for its easy maintenance and and is primarily targeted as the entry level motor in the light aviation hp product line offers more power while keeping the same weight. of the Rotax 4-stroke engine series complemented by additional high altitudes while delivering lower weight engines. series, the Rotax 915 iS engine offers more power, the best robustness. industry. The 80 hp version of the Rotax 912 series is available as features, for example, the engine management system. power-to-weight ratio in its class, full take-off power up to This engine series offers the best power to weight ratio in its class This series is available as non-certified version (Rotax 914 UL) non-certified (Rotax 912 UL) as well as certified version according 15,000 feet (4,570 m) and a service ceiling of 23,000 feet and is available as non-certified (Rotax 912 ULS) and certified This engine series is available as non-certified (Rotax 912 iS) as and certified version (Rotax 914 F) according to FAR 33 and to FAR 33 (Rotax 912 F) and JAR 22 (Rotax 912 A). (7,010 m). Available as ASTM compliant version (Rotax 915 iS) engine (Rotax 912 S) according to FAR33. well as certified version (Rotax 912 iSc) according to CS-E. JAR-E. as well as EASA CS-E certified (Rotax 915 iSc).

2-cylinder 4-cylinder Dual electronic ignition 4-cylinder Dual-electronic ignition 4-cylinder Electric starter 4-cylinder 2 4-cylinder Electric starter (12 or 24 volt) 2-stroke liquid-cooled engine 4-stroke liquid-/air-cooled engine Electric starter 4-stroke liquid-/air-cooled engine Electric starter 4-stroke liquid-/air-cooled engine Propeller speed reduction gearbox 4-stroke liquid-/air-cooled engine Dual electronic ignition 4-stroke liquid-/air-cooled engine Propeller speed reduction gearbox with opposed cylinders with horizontally opposed cylinders with intake with opposed cylinders Propeller speed reduction gearbox with opposed cylinders Propeller speed reduction gearbox with opposed cylinders Air intake system Electric starter Air intake system with Dual electronic ignition forced lubrication Dry sump forced lubrication Air intake system Dry sump forced lubrication TBO 2,000 hrs With turbo charger Propeller speed reduction gearbox Dry sump forced lubrication Turbocharger with stainless steel AlTITuDE PERfORMANCE - ISA CONDITIONS POWERINg yOuR with separate oil tank, automatic TBO 2,000 hrs with separate oil tank, automatic with separate oil tank, automatic with separate oil tank, automatic With automatic waste gate control exhaust Integrated water pump and thermostat adjustment by hydraulic valve tappet adjustment by hydraulic valve tappet TBO 2,000 hrs adjustment by hydraulic valve tappets Engine mount assembly adjustment by hydraulic valve Dry sump forced lubrication tappet Service ceiling of 23,000 feet Exhaust system 2 carburetors 2 carburetors Redundant electronic fuel injection Air intake system 100 with separate oil tank Redundant electronic fuel injection TBO 1,200 hrs Carburetors Mechanical fuel pump Mechanical fuel pump Engine management system Exhaust system ULTimATe FLigHT Automatic adjustment and ignition 80 by hydraulic valve tappet TBO 2,000 hrs Engine management system (EMS) 60

WEIghT kg lb WEIghT kg lb WEIghT kg lb WEIghT kg lb WEIghT kg lb WEIghT kg lb 40 Engine 29.1 64.0 Engine with propeller speed reduction Engine with propeller speed Engine with propeller speed reduction Engine with propeller speed Engine with gearbox, turbocharger, 55.4 122.0 56.6 124.5 63.6 140.2 64.0 140.8 84.6 186.4 gearbox i = 2.27 (opt. i = 2.43) reduction gearbox i = 2.43 gearbox i = 2.43 with overload clutch reduction gearbox i = 2.43 intercooler, cooling air baffle, wi- 20 Exhaust system 5.1 11.2 ring harness, sensors, flange with

Exhaust system 4.0 8.8 Exhaust system 4.0 8.8 Exhaust system 4.8 10.5 Exhaust system 4.0 8.8 Engine Power of [%] Maximum Cobntinuous Power 2 carburetors 1.8 4.0 overboost valve, air hoses, clamps, 0 5000 10000 15000 23000 30000 Overload clutch 1.7 3.7 Overload clutch 1.7 3.7 Overload clutch 1.7 3.7 magneto valve block with hoses, ECu, Electric starter 3.5 7.7 Altitude [ft] 912 ulS/S 912 iS 914 915 iS fusebox with regulators, oil tank, Engine suspension frame 2.0 4.4 Engine suspension frame 2.0 4.4 Engine mount 2.0 4.4 Engine suspension frame 2.0 3.7 PSRg* “B“ / i = 2.58 4.5 9.9 exhaust system. External alternator 3.0 6.6 External alternator 3.0 6.6 External alternator 3.0 6.6 External alternator 3.0 6.6 PSRg* “C“ / i = 2.62 / 3.0 / 3.47 / 4.0 8.0 17.6 Without fuel pumps assembly, radiator Air guide hood 0.8 1.8 Air guide hood 0.8 1.8 Air guide hood 0.4 0.8 Air guide hood 0.8 1.8 and oil cooler fuEl CONSuMPTION AND fuEl COSTS VS. 912 iS SPORT1) PSRg* “E“ / i = 2.62 / 3.0 / 3.47 / 4.0 11.2 24.7 30 *Propeller speed reduction gearbox Airbox 1.3 2.8 Airbox 1.3 2.8 fuel pumps assy 1.6 3.5

PERfORMANCE PERfORMANCE PERfORMANCE PERfORMANCE PERfORMANCE MAx. TAkE-Off PERfORMANCE 25 73.5 kW 100 hp 5800 1/min 48.0 kW 65 hp 6500 1/min. 59.6 kW 80 hp 5800 1/min. 73.5 kW 100 hp 5800 1/min. 72.0 kW** 98 hp 5500 1/min 84.5 kW 115 hp 5800 1/min. 104 kW 141 hp 5800 1/min. ] per flight hour

68.0 kW 92.5 hp 5000 1/min liter 20 TORquE TORquE TORquE TORquE TORquE MAx. CONTINuOuS PERfORMANCE 121 Nm 89 ft. lb. 5800 1/min 75 Nm 55.3 ft. lb. 6000 1/min. 103 Nm 75.9 ft. lb. 4800 1/min. 128 Nm 94 ft. lb. 5100 1/min. 125 Nm 92 ft. lb. 5500 1/min 144 Nm 106 ft. lb. 4900 1/min. 99 kW 135 hp 5500 1/min. 15 132 Nm*** 97 ft. lb. 5000 1/min

MAx RPM 6800 1/min. MAx RPM* 5800 1/min. MAx RPM* 5800 1/min. MAx RPM limited for max. 5 minutes 5800 1/min. MAx RPM* 5800 1/min. fuel Consumption [ STROkE BORE STROkE BORE STROkE BORE STROkE BORE STROkE BORE STROkE fuel Costs [Euro] 76.0 mm 2.99 in 64.0 mm 2.52 in 79.5 mm 3.13 in 61.0 mm 2.4 in 84.0 mm 3.31 in 61.0 mm 2.4 in 84.0 mm 3.31 in 61.0 mm 2.4 in 79.5 mm 3.13 in 61.0 mm 2.4 in 84.0 mm 3.31 in 61.0 mm 2.4 in per 100 flight hours DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl vs. 912 iS Sport 580 cm3 35.4 cu in min. MON 83 RON 91** 1211.2 cm3 73.9 cu in min. MON 83 RON 91* 1352 cm3 82.6 cu in min. MON 85 RON 95* 1352 cm3 82.6 cu in min. MON 85 RON 95* 1211.2 cm3 73.91 cu in min. MON 85 RON 95* 1352 cm3 82.5 cu in min. MON 85 RON 95 fuel type min. AkI 87** min. AkI 87* min. AkI 91* min. AkI 91* min. AkI 91* min. AkI 91 1) Information on the back side of the brochure

** leaded, unleaded, 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 Picture: Rotax 912 ulS - DCDI with options * leaded, unleaded, AVgAS 100ll Ethanol 10 ** max. continuous power at 5500 1/min * leaded, unleaded, AVgAS 100ll Ethanol 10 Picture: Rotax 914 ul - DCDI with options * leaded, unleaded, AVgAS 100ll Ethanol 10 Engine performance may vary depending on, among other things, general conditions, ambient temperature and altitude. *** MOgAS, no hydraulic governor ROTAx engineS 65 HP 582 UL 80 HP 912 UL/A/F 100 HP 912 ULS/S 100 HP 912 iS/iSc SPORT 115 H P 914 UL/F 141 HP 915 iS/iSc

Over 30,000 units of this popular Rotax 2-stroke engine have been The Rotax 912 series is well regarded for its reliability and efficiency In comparison to the 80 hp version of the Rotax 912 series the 100 The Rotax 912 iS Sport engine offers all well known advantages The turbo charged Rotax 914 series offers more performance at Based on the proven concept of the Rotax 912 / 914 engine sold. This engine type is well regarded for its easy maintenance and and is primarily targeted as the entry level motor in the light aviation hp product line offers more power while keeping the same weight. of the Rotax 4-stroke engine series complemented by additional high altitudes while delivering lower weight engines. series, the Rotax 915 iS engine offers more power, the best robustness. industry. The 80 hp version of the Rotax 912 series is available as features, for example, the engine management system. power-to-weight ratio in its class, full take-off power up to This engine series offers the best power to weight ratio in its class This series is available as non-certified version (Rotax 914 UL) non-certified (Rotax 912 UL) as well as certified version according 15,000 feet (4,570 m) and a service ceiling of 23,000 feet and is available as non-certified (Rotax 912 ULS) and certified This engine series is available as non-certified (Rotax 912 iS) as and certified version (Rotax 914 F) according to FAR 33 and to FAR 33 (Rotax 912 F) and JAR 22 (Rotax 912 A). (7,010 m). Available as ASTM compliant version (Rotax 915 iS) engine (Rotax 912 S) according to FAR33. well as certified version (Rotax 912 iSc) according to CS-E. JAR-E. as well as EASA CS-E certified (Rotax 915 iSc).

2-cylinder 4-cylinder Dual electronic ignition 4-cylinder Dual-electronic ignition 4-cylinder Electric starter 4-cylinder 2 carburetors 4-cylinder Electric starter (12 or 24 volt) 2-stroke liquid-cooled engine 4-stroke liquid-/air-cooled engine Electric starter 4-stroke liquid-/air-cooled engine Electric starter 4-stroke liquid-/air-cooled engine Propeller speed reduction gearbox 4-stroke liquid-/air-cooled engine Dual electronic ignition 4-stroke liquid-/air-cooled engine Propeller speed reduction gearbox with opposed cylinders with horizontally opposed cylinders with rotary valve intake with opposed cylinders Propeller speed reduction gearbox with opposed cylinders Propeller speed reduction gearbox with opposed cylinders Air intake system Electric starter Air intake system with intercooler Dual electronic ignition Dry sump forced lubrication Dry sump forced lubrication Air intake system Dry sump forced lubrication TBO 2,000 hrs With turbo charger Propeller speed reduction gearbox Dry sump forced lubrication Turbocharger with stainless steel AlTITuDE PERfORMANCE - ISA CONDITIONS POWERINg yOuR with separate oil tank, automatic TBO 2,000 hrs with separate oil tank, automatic with separate oil tank, automatic with separate oil tank, automatic With automatic waste gate control exhaust Integrated water pump and thermostat adjustment by hydraulic valve tappet adjustment by hydraulic valve tappet TBO 2,000 hrs adjustment by hydraulic valve tappets Engine mount assembly adjustment by hydraulic valve Dry sump forced lubrication tappet Service ceiling of 23,000 feet Exhaust system 2 carburetors 2 carburetors Redundant electronic fuel injection Air intake system 100 with separate oil tank Redundant electronic fuel injection TBO 1,200 hrs Carburetors Mechanical fuel pump Mechanical fuel pump Engine management system Exhaust system ULTimATe FLigHT Automatic adjustment and ignition 80 by hydraulic valve tappet TBO 2,000 hrs Engine management system (EMS) 60

WEIghT kg lb WEIghT kg lb WEIghT kg lb WEIghT kg lb WEIghT kg lb WEIghT kg lb 40 Engine 29.1 64.0 Engine with propeller speed reduction Engine with propeller speed Engine with propeller speed reduction Engine with propeller speed Engine with gearbox, turbocharger, 55.4 122.0 56.6 124.5 63.6 140.2 64.0 140.8 84.6 186.4 gearbox i = 2.27 (opt. i = 2.43) reduction gearbox i = 2.43 gearbox i = 2.43 with overload clutch reduction gearbox i = 2.43 intercooler, cooling air baffle, wi- 20 Exhaust system 5.1 11.2 ring harness, sensors, flange with

Exhaust system 4.0 8.8 Exhaust system 4.0 8.8 Exhaust system 4.8 10.5 Exhaust system 4.0 8.8 Engine Power of [%] Maximum Cobntinuous Power 2 carburetors 1.8 4.0 overboost valve, air hoses, clamps, 0 5000 10000 15000 23000 30000 Overload clutch 1.7 3.7 Overload clutch 1.7 3.7 Overload clutch 1.7 3.7 magneto valve block with hoses, ECu, Electric starter 3.5 7.7 Altitude [ft] 912 ulS/S 912 iS 914 915 iS fusebox with regulators, oil tank, Engine suspension frame 2.0 4.4 Engine suspension frame 2.0 4.4 Engine mount 2.0 4.4 Engine suspension frame 2.0 3.7 PSRg* “B“ / i = 2.58 4.5 9.9 exhaust system. External alternator 3.0 6.6 External alternator 3.0 6.6 External alternator 3.0 6.6 External alternator 3.0 6.6 PSRg* “C“ / i = 2.62 / 3.0 / 3.47 / 4.0 8.0 17.6 Without fuel pumps assembly, radiator Air guide hood 0.8 1.8 Air guide hood 0.8 1.8 Air guide hood 0.4 0.8 Air guide hood 0.8 1.8 and oil cooler fuEl CONSuMPTION AND fuEl COSTS VS. 912 iS SPORT1) PSRg* “E“ / i = 2.62 / 3.0 / 3.47 / 4.0 11.2 24.7 30 *Propeller speed reduction gearbox Airbox 1.3 2.8 Airbox 1.3 2.8 fuel pumps assy 1.6 3.5

PERfORMANCE PERfORMANCE PERfORMANCE PERfORMANCE PERfORMANCE MAx. TAkE-Off PERfORMANCE 25 73.5 kW 100 hp 5800 1/min 48.0 kW 65 hp 6500 1/min. 59.6 kW 80 hp 5800 1/min. 73.5 kW 100 hp 5800 1/min. 72.0 kW** 98 hp 5500 1/min 84.5 kW 115 hp 5800 1/min. 104 kW 141 hp 5800 1/min. ] per flight hour

68.0 kW 92.5 hp 5000 1/min liter 20 TORquE TORquE TORquE TORquE TORquE MAx. CONTINuOuS PERfORMANCE 121 Nm 89 ft. lb. 5800 1/min 75 Nm 55.3 ft. lb. 6000 1/min. 103 Nm 75.9 ft. lb. 4800 1/min. 128 Nm 94 ft. lb. 5100 1/min. 125 Nm 92 ft. lb. 5500 1/min 144 Nm 106 ft. lb. 4900 1/min. 99 kW 135 hp 5500 1/min. 15 132 Nm*** 97 ft. lb. 5000 1/min

MAx RPM 6800 1/min. MAx RPM* 5800 1/min. MAx RPM* 5800 1/min. MAx RPM limited for max. 5 minutes 5800 1/min. MAx RPM* 5800 1/min. fuel Consumption [ BORE STROkE BORE STROkE BORE STROkE BORE STROkE BORE STROkE BORE STROkE fuel Costs [Euro] 76.0 mm 2.99 in 64.0 mm 2.52 in 79.5 mm 3.13 in 61.0 mm 2.4 in 84.0 mm 3.31 in 61.0 mm 2.4 in 84.0 mm 3.31 in 61.0 mm 2.4 in 79.5 mm 3.13 in 61.0 mm 2.4 in 84.0 mm 3.31 in 61.0 mm 2.4 in per 100 flight hours DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl vs. 912 iS Sport 580 cm3 35.4 cu in min. MON 83 RON 91** 1211.2 cm3 73.9 cu in min. MON 83 RON 91* 1352 cm3 82.6 cu in min. MON 85 RON 95* 1352 cm3 82.6 cu in min. MON 85 RON 95* 1211.2 cm3 73.91 cu in min. MON 85 RON 95* 1352 cm3 82.5 cu in min. MON 85 RON 95 fuel type min. AkI 87** min. AkI 87* min. AkI 91* min. AkI 91* min. AkI 91* min. AkI 91 1) Information on the back side of the brochure

** leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 Picture: Rotax 912 ulS - DCDI with options * leaded, unleaded, AVgAS 100ll Ethanol 10 ** max. continuous power at 5500 1/min * leaded, unleaded, AVgAS 100ll Ethanol 10 Picture: Rotax 914 ul - DCDI with options * leaded, unleaded, AVgAS 100ll Ethanol 10 Engine performance may vary depending on, among other things, general conditions, ambient temperature and altitude. *** MOgAS, no hydraulic governor ROTAx engineS 65 HP 582 UL 80 HP 912 UL/A/F 100 HP 912 ULS/S 100 HP 912 iS/iSc SPORT 115 H P 914 UL/F 141 HP 915 iS/iSc

Over 30,000 units of this popular Rotax 2-stroke engine have been The Rotax 912 series is well regarded for its reliability and efficiency In comparison to the 80 hp version of the Rotax 912 series the 100 The Rotax 912 iS Sport engine offers all well known advantages The turbo charged Rotax 914 series offers more performance at Based on the proven concept of the Rotax 912 / 914 engine sold. This engine type is well regarded for its easy maintenance and and is primarily targeted as the entry level motor in the light aviation hp product line offers more power while keeping the same weight. of the Rotax 4-stroke engine series complemented by additional high altitudes while delivering lower weight engines. series, the Rotax 915 iS engine offers more power, the best robustness. industry. The 80 hp version of the Rotax 912 series is available as features, for example, the engine management system. power-to-weight ratio in its class, full take-off power up to This engine series offers the best power to weight ratio in its class This series is available as non-certified version (Rotax 914 UL) non-certified (Rotax 912 UL) as well as certified version according 15,000 feet (4,570 m) and a service ceiling of 23,000 feet and is available as non-certified (Rotax 912 ULS) and certified This engine series is available as non-certified (Rotax 912 iS) as and certified version (Rotax 914 F) according to FAR 33 and to FAR 33 (Rotax 912 F) and JAR 22 (Rotax 912 A). (7,010 m). Available as ASTM compliant version (Rotax 915 iS) engine (Rotax 912 S) according to FAR33. well as certified version (Rotax 912 iSc) according to CS-E. JAR-E. as well as EASA CS-E certified (Rotax 915 iSc).

2-cylinder 4-cylinder Dual electronic ignition 4-cylinder Dual-electronic ignition 4-cylinder Electric starter 4-cylinder 2 carburetors 4-cylinder Electric starter (12 or 24 volt) 2-stroke liquid-cooled engine 4-stroke liquid-/air-cooled engine Electric starter 4-stroke liquid-/air-cooled engine Electric starter 4-stroke liquid-/air-cooled engine Propeller speed reduction gearbox 4-stroke liquid-/air-cooled engine Dual electronic ignition 4-stroke liquid-/air-cooled engine Propeller speed reduction gearbox with opposed cylinders with horizontally opposed cylinders with rotary valve intake with opposed cylinders Propeller speed reduction gearbox with opposed cylinders Propeller speed reduction gearbox with opposed cylinders Air intake system Electric starter Air intake system with intercooler Dual electronic ignition Dry sump forced lubrication Dry sump forced lubrication Air intake system Dry sump forced lubrication TBO 2,000 hrs With turbo charger Propeller speed reduction gearbox Dry sump forced lubrication Turbocharger with stainless steel AlTITuDE PERfORMANCE - ISA CONDITIONS POWERINg yOuR with separate oil tank, automatic TBO 2,000 hrs with separate oil tank, automatic with separate oil tank, automatic with separate oil tank, automatic With automatic waste gate control exhaust Integrated water pump and thermostat adjustment by hydraulic valve tappet adjustment by hydraulic valve tappet TBO 2,000 hrs adjustment by hydraulic valve tappets Engine mount assembly adjustment by hydraulic valve Dry sump forced lubrication tappet Service ceiling of 23,000 feet Exhaust system 2 carburetors 2 carburetors Redundant electronic fuel injection Air intake system 100 with separate oil tank Redundant electronic fuel injection TBO 1,200 hrs Carburetors Mechanical fuel pump Mechanical fuel pump Engine management system Exhaust system ULTimATe FLigHT Automatic adjustment and ignition 80 by hydraulic valve tappet TBO 2,000 hrs Engine management system (EMS) 60

WEIghT kg lb WEIghT kg lb WEIghT kg lb WEIghT kg lb WEIghT kg lb WEIghT kg lb 40 Engine 29.1 64.0 Engine with propeller speed reduction Engine with propeller speed Engine with propeller speed reduction Engine with propeller speed Engine with gearbox, turbocharger, 55.4 122.0 56.6 124.5 63.6 140.2 64.0 140.8 84.6 186.4 gearbox i = 2.27 (opt. i = 2.43) reduction gearbox i = 2.43 gearbox i = 2.43 with overload clutch reduction gearbox i = 2.43 intercooler, cooling air baffle, wi- 20 Exhaust system 5.1 11.2 ring harness, sensors, flange with

Exhaust system 4.0 8.8 Exhaust system 4.0 8.8 Exhaust system 4.8 10.5 Exhaust system 4.0 8.8 Engine Power of [%] Maximum Cobntinuous Power 2 carburetors 1.8 4.0 overboost valve, air hoses, clamps, 0 5000 10000 15000 23000 30000 Overload clutch 1.7 3.7 Overload clutch 1.7 3.7 Overload clutch 1.7 3.7 magneto valve block with hoses, ECu, Electric starter 3.5 7.7 Altitude [ft] 912 ulS/S 912 iS 914 915 iS fusebox with regulators, oil tank, Engine suspension frame 2.0 4.4 Engine suspension frame 2.0 4.4 Engine mount 2.0 4.4 Engine suspension frame 2.0 3.7 PSRg* “B“ / i = 2.58 4.5 9.9 exhaust system. External alternator 3.0 6.6 External alternator 3.0 6.6 External alternator 3.0 6.6 External alternator 3.0 6.6 PSRg* “C“ / i = 2.62 / 3.0 / 3.47 / 4.0 8.0 17.6 Without fuel pumps assembly, radiator Air guide hood 0.8 1.8 Air guide hood 0.8 1.8 Air guide hood 0.4 0.8 Air guide hood 0.8 1.8 and oil cooler fuEl CONSuMPTION AND fuEl COSTS VS. 912 iS SPORT1) PSRg* “E“ / i = 2.62 / 3.0 / 3.47 / 4.0 11.2 24.7 30 *Propeller speed reduction gearbox Airbox 1.3 2.8 Airbox 1.3 2.8 fuel pumps assy 1.6 3.5

PERfORMANCE PERfORMANCE PERfORMANCE PERfORMANCE PERfORMANCE MAx. TAkE-Off PERfORMANCE 25 73.5 kW 100 hp 5800 1/min 48.0 kW 65 hp 6500 1/min. 59.6 kW 80 hp 5800 1/min. 73.5 kW 100 hp 5800 1/min. 72.0 kW** 98 hp 5500 1/min 84.5 kW 115 hp 5800 1/min. 104 kW 141 hp 5800 1/min. ] per flight hour

68.0 kW 92.5 hp 5000 1/min liter 20 TORquE TORquE TORquE TORquE TORquE MAx. CONTINuOuS PERfORMANCE 121 Nm 89 ft. lb. 5800 1/min 75 Nm 55.3 ft. lb. 6000 1/min. 103 Nm 75.9 ft. lb. 4800 1/min. 128 Nm 94 ft. lb. 5100 1/min. 125 Nm 92 ft. lb. 5500 1/min 144 Nm 106 ft. lb. 4900 1/min. 99 kW 135 hp 5500 1/min. 15 132 Nm*** 97 ft. lb. 5000 1/min

MAx RPM 6800 1/min. MAx RPM* 5800 1/min. MAx RPM* 5800 1/min. MAx RPM limited for max. 5 minutes 5800 1/min. MAx RPM* 5800 1/min. fuel Consumption [ BORE STROkE BORE STROkE BORE STROkE BORE STROkE BORE STROkE BORE STROkE fuel Costs [Euro] 76.0 mm 2.99 in 64.0 mm 2.52 in 79.5 mm 3.13 in 61.0 mm 2.4 in 84.0 mm 3.31 in 61.0 mm 2.4 in 84.0 mm 3.31 in 61.0 mm 2.4 in 79.5 mm 3.13 in 61.0 mm 2.4 in 84.0 mm 3.31 in 61.0 mm 2.4 in per 100 flight hours DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl vs. 912 iS Sport 580 cm3 35.4 cu in min. MON 83 RON 91** 1211.2 cm3 73.9 cu in min. MON 83 RON 91* 1352 cm3 82.6 cu in min. MON 85 RON 95* 1352 cm3 82.6 cu in min. MON 85 RON 95* 1211.2 cm3 73.91 cu in min. MON 85 RON 95* 1352 cm3 82.5 cu in min. MON 85 RON 95 fuel type min. AkI 87** min. AkI 87* min. AkI 91* min. AkI 91* min. AkI 91* min. AkI 91 1) Information on the back side of the brochure

** leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 Picture: Rotax 912 ulS - DCDI with options * leaded, unleaded, AVgAS 100ll Ethanol 10 ** max. continuous power at 5500 1/min * leaded, unleaded, AVgAS 100ll Ethanol 10 Picture: Rotax 914 ul - DCDI with options * leaded, unleaded, AVgAS 100ll Ethanol 10 Engine performance may vary depending on, among other things, general conditions, ambient temperature and altitude. *** MOgAS, no hydraulic governor ROTAx engineS 65 HP 582 UL 80 HP 912 UL/A/F 100 HP 912 ULS/S 100 HP 912 iS/iSc SPORT 115 H P 914 UL/F 141 HP 915 iS/iSc

Over 30,000 units of this popular Rotax 2-stroke engine have been The Rotax 912 series is well regarded for its reliability and efficiency In comparison to the 80 hp version of the Rotax 912 series the 100 The Rotax 912 iS Sport engine offers all well known advantages The turbo charged Rotax 914 series offers more performance at Based on the proven concept of the Rotax 912 / 914 engine sold. This engine type is well regarded for its easy maintenance and and is primarily targeted as the entry level motor in the light aviation hp product line offers more power while keeping the same weight. of the Rotax 4-stroke engine series complemented by additional high altitudes while delivering lower weight engines. series, the Rotax 915 iS engine offers more power, the best robustness. industry. The 80 hp version of the Rotax 912 series is available as features, for example, the engine management system. power-to-weight ratio in its class, full take-off power up to This engine series offers the best power to weight ratio in its class This series is available as non-certified version (Rotax 914 UL) non-certified (Rotax 912 UL) as well as certified version according 15,000 feet (4,570 m) and a service ceiling of 23,000 feet and is available as non-certified (Rotax 912 ULS) and certified This engine series is available as non-certified (Rotax 912 iS) as and certified version (Rotax 914 F) according to FAR 33 and to FAR 33 (Rotax 912 F) and JAR 22 (Rotax 912 A). (7,010 m). Available as ASTM compliant version (Rotax 915 iS) engine (Rotax 912 S) according to FAR33. well as certified version (Rotax 912 iSc) according to CS-E. JAR-E. as well as EASA CS-E certified (Rotax 915 iSc).

2-cylinder 4-cylinder Dual electronic ignition 4-cylinder Dual-electronic ignition 4-cylinder Electric starter 4-cylinder 2 carburetors 4-cylinder Electric starter (12 or 24 volt) 2-stroke liquid-cooled engine 4-stroke liquid-/air-cooled engine Electric starter 4-stroke liquid-/air-cooled engine Electric starter 4-stroke liquid-/air-cooled engine Propeller speed reduction gearbox 4-stroke liquid-/air-cooled engine Dual electronic ignition 4-stroke liquid-/air-cooled engine Propeller speed reduction gearbox with opposed cylinders with horizontally opposed cylinders with rotary valve intake with opposed cylinders Propeller speed reduction gearbox with opposed cylinders Propeller speed reduction gearbox with opposed cylinders Air intake system Electric starter Air intake system with intercooler Dual electronic ignition Dry sump forced lubrication Dry sump forced lubrication Air intake system Dry sump forced lubrication TBO 2,000 hrs With turbo charger Propeller speed reduction gearbox Dry sump forced lubrication Turbocharger with stainless steel AlTITuDE PERfORMANCE - ISA CONDITIONS POWERINg yOuR with separate oil tank, automatic TBO 2,000 hrs with separate oil tank, automatic with separate oil tank, automatic with separate oil tank, automatic With automatic waste gate control exhaust Integrated water pump and thermostat adjustment by hydraulic valve tappet adjustment by hydraulic valve tappet TBO 2,000 hrs adjustment by hydraulic valve tappets Engine mount assembly adjustment by hydraulic valve Dry sump forced lubrication tappet Service ceiling of 23,000 feet Exhaust system 2 carburetors 2 carburetors Redundant electronic fuel injection Air intake system 100 with separate oil tank Redundant electronic fuel injection TBO 1,200 hrs Carburetors Mechanical fuel pump Mechanical fuel pump Engine management system Exhaust system ULTimATe FLigHT Automatic adjustment and ignition 80 by hydraulic valve tappet TBO 2,000 hrs Engine management system (EMS) 60

WEIghT kg lb WEIghT kg lb WEIghT kg lb WEIghT kg lb WEIghT kg lb WEIghT kg lb 40 Engine 29.1 64.0 Engine with propeller speed reduction Engine with propeller speed Engine with propeller speed reduction Engine with propeller speed Engine with gearbox, turbocharger, 55.4 122.0 56.6 124.5 63.6 140.2 64.0 140.8 84.6 186.4 gearbox i = 2.27 (opt. i = 2.43) reduction gearbox i = 2.43 gearbox i = 2.43 with overload clutch reduction gearbox i = 2.43 intercooler, cooling air baffle, wi- 20 Exhaust system 5.1 11.2 ring harness, sensors, flange with

Exhaust system 4.0 8.8 Exhaust system 4.0 8.8 Exhaust system 4.8 10.5 Exhaust system 4.0 8.8 Engine Power of [%] Maximum Cobntinuous Power 2 carburetors 1.8 4.0 overboost valve, air hoses, clamps, 0 5000 10000 15000 23000 30000 Overload clutch 1.7 3.7 Overload clutch 1.7 3.7 Overload clutch 1.7 3.7 magneto valve block with hoses, ECu, Electric starter 3.5 7.7 Altitude [ft] 912 ulS/S 912 iS 914 915 iS fusebox with regulators, oil tank, Engine suspension frame 2.0 4.4 Engine suspension frame 2.0 4.4 Engine mount 2.0 4.4 Engine suspension frame 2.0 3.7 PSRg* “B“ / i = 2.58 4.5 9.9 exhaust system. External alternator 3.0 6.6 External alternator 3.0 6.6 External alternator 3.0 6.6 External alternator 3.0 6.6 PSRg* “C“ / i = 2.62 / 3.0 / 3.47 / 4.0 8.0 17.6 Without fuel pumps assembly, radiator Air guide hood 0.8 1.8 Air guide hood 0.8 1.8 Air guide hood 0.4 0.8 Air guide hood 0.8 1.8 and oil cooler fuEl CONSuMPTION AND fuEl COSTS VS. 912 iS SPORT1) PSRg* “E“ / i = 2.62 / 3.0 / 3.47 / 4.0 11.2 24.7 30 *Propeller speed reduction gearbox Airbox 1.3 2.8 Airbox 1.3 2.8 fuel pumps assy 1.6 3.5

PERfORMANCE PERfORMANCE PERfORMANCE PERfORMANCE PERfORMANCE MAx. TAkE-Off PERfORMANCE 25 73.5 kW 100 hp 5800 1/min 48.0 kW 65 hp 6500 1/min. 59.6 kW 80 hp 5800 1/min. 73.5 kW 100 hp 5800 1/min. 72.0 kW** 98 hp 5500 1/min 84.5 kW 115 hp 5800 1/min. 104 kW 141 hp 5800 1/min. ] per flight hour

68.0 kW 92.5 hp 5000 1/min liter 20 TORquE TORquE TORquE TORquE TORquE MAx. CONTINuOuS PERfORMANCE 121 Nm 89 ft. lb. 5800 1/min 75 Nm 55.3 ft. lb. 6000 1/min. 103 Nm 75.9 ft. lb. 4800 1/min. 128 Nm 94 ft. lb. 5100 1/min. 125 Nm 92 ft. lb. 5500 1/min 144 Nm 106 ft. lb. 4900 1/min. 99 kW 135 hp 5500 1/min. 15 132 Nm*** 97 ft. lb. 5000 1/min

MAx RPM 6800 1/min. MAx RPM* 5800 1/min. MAx RPM* 5800 1/min. MAx RPM limited for max. 5 minutes 5800 1/min. MAx RPM* 5800 1/min. fuel Consumption [ BORE STROkE BORE STROkE BORE STROkE BORE STROkE BORE STROkE BORE STROkE fuel Costs [Euro] 76.0 mm 2.99 in 64.0 mm 2.52 in 79.5 mm 3.13 in 61.0 mm 2.4 in 84.0 mm 3.31 in 61.0 mm 2.4 in 84.0 mm 3.31 in 61.0 mm 2.4 in 79.5 mm 3.13 in 61.0 mm 2.4 in 84.0 mm 3.31 in 61.0 mm 2.4 in per 100 flight hours DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl DISPlACEMENT fuEl vs. 912 iS Sport 580 cm3 35.4 cu in min. MON 83 RON 91** 1211.2 cm3 73.9 cu in min. MON 83 RON 91* 1352 cm3 82.6 cu in min. MON 85 RON 95* 1352 cm3 82.6 cu in min. MON 85 RON 95* 1211.2 cm3 73.91 cu in min. MON 85 RON 95* 1352 cm3 82.5 cu in min. MON 85 RON 95 fuel type min. AkI 87** min. AkI 87* min. AkI 91* min. AkI 91* min. AkI 91* min. AkI 91 1) Information on the back side of the brochure

** leaded, unleaded, AVgAS 100ll Ethanol 10 * leaded, unleaded, AVgAS 100ll Ethanol 10 Picture: Rotax 912 ulS - DCDI with options * leaded, unleaded, AVgAS 100ll Ethanol 10 ** max. continuous power at 5500 1/min * leaded, unleaded, AVgAS 100ll Ethanol 10 Picture: Rotax 914 ul - DCDI with options * leaded, unleaded, AVgAS 100ll Ethanol 10 Engine performance may vary depending on, among other things, general conditions, ambient temperature and altitude. *** MOgAS, no hydraulic governor our collaborations with international aircraft manufacturers

OEM statements B enefits down to earth fir st in the world s tate of the art DTA has been working with ROTAX for more than 20 years now, and we Rotax aircraft engines represent the state of the art in design, reliability have been the first trike manufacturer in the world to install a Rotax 912 and customer service. Our relationship with Rotax dates back to the mid engine for trike aircrafts that flew round the world, back in 1995, so the 1980’s, we sell our aircraft worldwide with Rotax and with confidence. relationship that we have with Rotax has been more than profitable for us. We have sold our aircraft to over 30 countries and can always rely on the DTA always had a reputation for quality and reliability, so we do not even exceptional reliability and worldwide customer service that Rotax delivers. think of changing our engine provider since we always talk to people that Russell Duncan share the same passion for flying. Rotax has always been receptive to our Director, Airborne needs, so it is really a win-win business between us. George Monier DTA sas Opi t mized cost Rotax engines have the perfect power-to-weight balance and and an effi- cient power production to optimize cost of ownership for private pilots as out standing well as for flight schools and other commercial usage. The company offers In one word: outstanding! This is one of the greatest developments in a global network to support customers with technical advise, spares, ser- aviation engines since decades. The 912 series and the 915 iS are vices and AOG support everywhere to keep them flying. all bringing the best from everything Rotax has built over the last 30 years: Ivo Boscarol weight/power ratio, fuel economy, power, performances, high altitude be- CEO, Pipistrel d.o.o. Ajdovscina nefits, excellent cost of ownership value... Paolo Pascale CEO, Costruzioni Aeronautiche S.r.l. be st product on the market We choose Rotax because we have known it for decades, even before aircraft engines, we knew Rotax for motorcycle engines. We believe it is the perfect fit currently the best product on the market in terms of reliability. The high power to weight ratio provided by the 9 series Rotax is critical Our company rejects the installation of handmade products or derivatives, to the overall twin engine design of the AirCam. Add to that excellent re- Rotax has the technical and technological skills to meet our reliability and liability, quite operation and very good fuel efficiency and you have the safety standards. perfect fit. And last but not least, we have a great feeling with the Italian distributor Phillip Lockwood Luciano Sorlini S.p.A., they give us an excellent support, they are always AirCam & Lockwood Aviation Supply ready to respond with courtesy, professionalism and friendliness to our requests. Razzano Tancredi Had n s down the winner CEO, I.C.P. srl When it came to ICON choosing a powerplant for the A5 Aircraft based on power-to-weight, reliability, availability, and price ... the Rotax 912 iS was hands down the winner. Kirk Hawkins CEO, ICON Aircraft Inc. our collaborations with international aircraft manufacturers

Aerospool / WT9 Dynamics / Rotax 912 ULS2 Air Creation / Skypper / Rotax 912 ULS Autogyro / MTO Sport 2017 / Rotax 912 ULS, 914 UL, 915 iS

BRM Aero/Bristell NG 5/Rotax 912 iS Sport, 912 ULS, 914 UL, 915 iS Diamond / DA-20 Katana / 912 S, 912 iSc Sport I.C.P. / Savannah S / Rotax 912 ULS, 912 iS Sport

Issoire Aviation / APM 41 Simba / Rotax 915 iS, 915 iSc Magni Gyro / M24 Orion / Rotax 914 UL Pipistrel / Virus SW / Rotax 912 iS Sport eon Mitton D Photo ©

Progressive Aerodyne / Searey / Rotax 915 iS The Airplane Factory / Sling 4 / Rotax 914 UL, 915 iS Tecnam / P2006T / Rotax 912 S

Tecnam / P2008JC / Rotax 912 S TL Ultralights / Sting S4 / Rotax 912 iS Sport, 912 ULS, 914 UL Van‘s Aircraft / RV 12i / 912 iS Sport, 912 ULS international awards and our company history awa rds & Certificates Our awards are cornerstones of trust, our certificates are important milestones in the commercialization of new aircraft engines. Awards C eertificat s

BRP-Rotax was awarded 1st place Innovation Award in the category Aero Engines by Best Brands 2009 DOA / POA Important milestones for the Rotax aircraft engines business were to meet BRP-Rotax was awarded the Dr. August Raspet Memorial Award the Design and Production certification standards of the European Aviati- for Outstanding Contributions to the Advancement of Light on Safety Agency (EASA). The Design Organisation Approval (DOA) and Aircraft Design by the Experimental Aircraft Association (EAA) Production Organisation Approval (POA) are valid for all types of certified in 2013 aircraft engines.

Rotax 912 iS was awarded the Most Advanced Powertrain Concept by fliegermagazin 2013 E ASA TYPE CERTIFICATE The EASA Type Certificate (TC) allows BRP to produce certified engines Rotax 912 iS was awarded the Innovation Award for the European market and to make changes on certified piston engines. in the category Powertrain of the Future by aerokurier 2014 These are important milestones in the commercialization of new aircraft engines. The European Aviation Safety Agency (EASA) promotes the hig- Rotax 912 iS was awarded the Innovation Award hest standards of safety and environmental protection in civil aviation in in the category Powertrain of the Future by aerokurier 2015 Europe and worldwide. Rotax 915 iS was awarded in the category Best Powertrain ASTM Concept by fliegermagazin 2016 ASTM (American Society for Testing and Materials) is an international standard organization that develops and publishes voluntary consensus Rotax 915 iS was awarded the Innovation Award and technical standards for a wide range of materials, products, systems in the category Powertrain of the Future by aerokurier 2017 and services. All Rotax 4-stroke aircraft engines and the 2-stroke Ro- tax 582 UL comply with the ASTM F2339 standard published by ASTM (Standard Practice for Design and Manufacture of Reciprocating Spark Ignition Engines for Light Sport Aircraft).

COMPLIANCE STATEMENT - DECLARATION OF COMPLIANCE to ASTM F2339-06

Engine Type: Engine s/n:

References:

1. ASTM F2339-06

2. Serial Numbers (since ASTM has been established for ROTAX Aircraft Engines) 912 A ...... from S/N 4410660 on 912 F ...... from S/N 4412888 on 912 S ...... from S/N 4923163 on 912 UL ...... from S/N 4407160 on 912 ULS ...... from S/N 5644817 on 912 ULSFR ...... from S/N 4430116 on 912 iS / iS Sport...... from S/N 4417078 on 912 iSc Sport...... from S/N 4417412 on 914 F ...... from S/N 4420471 on 914 UL ...... from S/N 4419024 on 915 iS A ...... from S/N 9132042 on

BRP-Rotax GmbH & Co KG hereby declares that the or part of thereof as described in the statement of compliance confirms to the applicable ASTM F2339-06 standard.

No features or characteristics are found which would make the engine unsafe provided it is installed, operated and maintained in accordance with instructions and limitations as defined by BRP-Rotax approved documentation.

The product complies with the ASTM F2339-06 standard based on BRP’s quality system for record keeping and instructions for continued airworthiness.

Dr. Thomas Hametner Maximilian Feischl Head of Design Organisation Accountable Manager

Gunskirchen, 22.11.2017

BRP-Rotax GmbH & Co KG I Rotaxstraße 1 I 4623 Gunskirchen I Austria

FB 16-012-1/M www.flyrotax.com international awards and our company history

A s time flies by the company history of brp-rotax spotlight on rotax aircraft engines For almost a century, we have dedicated ourselves to passion and innovation. It’s about what we build and the emotions we provide. Be a part of this unique heritage of ingenuity and excellence, benefit from our experience, start your own adventure. 1920 Founding of Rotax-Werk AG in Dresden, 1947 Relocation to Gunskirchen, Austria Bombardier aquires Rotax-Werk AG, 1970 becoming Bombardier-Rotax GmbH 1975 Certification of the first Rotax aircraft engine (Rotax 642) Rotax 502 and 505 ultralight engines produced 1978 (based on engine 503) 1984 Start of development of Rotax 912 engine 1989 Type Certificate for Rotax 912 A 1994 Type Certificate for Rotax 912 F 1996 Type Certificate for Rotax 914 F 1998 Type Certificate for Rotax 912 S 2003 Design Organisation Approval by EASA 2005 Production Organisation Approval by EASA Rotax 912/914 engine series compliant to 2005 Light Sport Aircraft Norm ASTM 2006 engine compliant to Light Sport Aircraft Norm ASTM 2012 Launch of Rotax 912 iS aircraft engine 2013 BRP Inc. becomes a public company 2014 Launch of Rotax 912 iS Sport aircraft engine 2017 Launch of Rotax 915 iS engine M ake your free time your best Time atana / 912 S, iSc Sport K A-20 D iamond / Picture: Alexander Schrempf D

We are dedicated to continually finding new and better ways to help you enjoy your favourite powersports.

Our desire to thrill is paired with an emphasis on and pilot responsibility, placing per- sonal safety above all else. So that each outing can be the most enjoyable, and memorable experience possible. www.flyrotax.com

1) Based on cruise power setting at 5,000 rpm at 5,000 ft MSL and comparable fuel BRP-Rotax GmbH & Co KG reserves the right at any time to discontinue or change specifi- consumption according to the following sources (Feb. 2012): cations, prices, designs, features, models or equipment without incurring obligation. Engi- www.tcmlink.com/EngSpecSheetDocs/O200B.pdf, www.lycoming.com/news-and-events/ ne performance may vary depending on, among other things, general conditions, ambient pdfs/233-engine.pdf, www.jabiru.net.au/images/6-cylinder/3300%20Aero%20Engi- temperature and altitude. These technical data and the information contained therein are ne%20Flyer.pdf, Costs of fuel: Mogas EUR 1.60 / liter and Avgas EUR 2.408 / liter - air- property of BRP- Rotax GmbH & Co KG and must not be reproduced, neither entirely nor port Wels Februray 1, 2012 partially, and passed on to third parties without previous consent in writing by BRP-Rotax GmbH & Co KG. For information only – without commitment to subsequent modifications. Note: Rotax UL aircraft engines do not comply with federal safety regulations for standard aircraft. This engine is for use in experimental and ultralight uncertified aircraft only and © 2018 BRP-Rotax GmbH & Co KG. All rights reserved. ®, TM and the BRP logo are only in circumstances in which an engine failure will not compromise safety. Before opera- trademarks of Bombardier Recreational Products Inc. (BRP) or its affiliates. All other tra- ting the engine read operator‘s manual. Information is available from your local authorized demarks are the property of their respective owners. Rotax-distributor.