ENGINE OPTIONS

• 95 hp at 5500 rpm; 84 mm bore; 61 mm

stroke; 1352 cm3 displacement; 10.5:1

compression ratio

• Fuel: 89 — 93 octane, unleaded gasoline

(best); orAvgas 100 LL

• Fuel consumption: 4.7 gallons (U.S.) per

hour at 75% load

• TBO: 1500 hour

Rotax 914

The potent turbo-charged 914 is the engine of choice for high-altitude flight operations

• Four-cylinder, four stroke liquid/air cooled engine with opposed cylinders, with turbo charger, dry sump forced lubrication with separate 3 liter oil tank, automatic adjustment by hydraulic valve tappet, 2 CD carburetors, electronic dual ignition, electric starter, exhaust system, integrated reduction gear 1=2.273.

• 115 hp at 5,800 rpm; 79.5 mm bore; 61 mm stroke; 1211.2 cm³ displacement; 9.0:1 compression ratio

• Fuel: 89 — 93 octane, unleaded gasoline (best); orAvgas 100 LL

• Fuel consumption: 3.2 gallons (U.S.) per hour

• TBO: 1500 hours

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