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Choose an Engine to start Configuration

916iS RC / iS RC C24 160 HP

Four-stroke piston engine with four liquid and air-cooled cylinders
Redundant electronic fuel injection and ignition, eco mode
Turbocharger, stainless steel exhaust
Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappets
Engine management system (EMS)
Electric starter (12 or 24 Volt)
Propeller speed reduction gearbox
Intercooler
TBO 2,000 hrs
Maximum operating altitude 23,000 feet
Start Configuration for quote >>>>

915 iS/ iS C24 141 HP

Four-stroke piston engine with four liquid and air-cooled cylinders
Redundant electronic fuel injection and ignition, eco mode
Turbocharger, stainless steel exhaust
Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappets
Engine management system (EMS)
Electric starter (12 or 24 volt)
Propeller speed reduction gearbox
Air intake system / intercooler
TBO 1,200 hrs
Maximum operating altitude 23.000 feet
Start Configuration for quote >>>>

912 iS / 912 iS C24 / 912 iS RC 100 HP

Four-stroke piston engine with four liquid- and air-cooled cylinders
Redundant electronic fuel injection and ignition, eco mode
EMS and propeller speed reduction gearbox
Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappets
Electric starter
Air intake system
TBO 2,000 hrs
Start Configuration for quote >>>>

914 UL 115 HP

Four-stroke piston engine with four liquid and air-cooled cylinders
Turbocharger / Automatic wastegate control
Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet
Dual electronic ignition / Electric starter
Propeller speed reduction gearbox
Air intake system / Exhaust system
TBO 2,000 hrs
Start Configuration for quote >>>>

912 ULS 100 HP

Four-stroke piston engine with four liquid and air-cooled cylinders
Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet
2 carburetors
Mechanical fuel pump
Dual-electronic ignition
Electric starter
Propeller speed reduction gearbox
Air intake system
TBO 2,000 hrs
Start Configuration for quote >>>>

912 UL 80 HP

Four-stroke piston engine with four liquid and air-cooled cylinders
Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet
The lightest engine in the Rotax aircraft engine portfolio
2 carburetors
Mechanical fuel pump
Dual electronic ignition
Electric starter
Propeller speed reduction gearbox
TBO 2,000 hrs
Start Configuration for quote >>>>

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