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Rotax 912S (ULS2) Engine
The
newest addition to the Rotax line adds extra power for those who require
it.
Four-cylinder, four-stroke liquid/air cooled engine with opposed cylinders,
dry sump forced lubrication with separate 3 liter oil tank, automatic
adjustment by hydraulic valve tappet, 2 CD carburetors, mechanical fuel
pump, electronic dual ignition, electric starter, integrated reduction
gear 1=2.43
95 hp at 5500 rpm; 84 mm bore; 61 mm stroke; 1352 cm displacement; 10.5:1
compression ratio
Fuel: 89 - 93 octane, unleaded gasoline (best); or Avgas 100 LL
Fuel consumption: 4.7 gallons (U.S.) per hour at 75% load
TBO: 1500 hour
Rotax
914 (UL2) Turbo Engine
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); or Avgas 100 LL
Fuel consumption: 3.2 gallons (U.S.) per hour
TBO: 1200 hours
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