Properties (48)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
engine
|
| gptkbp:application |
light aircraft
|
| gptkbp:certifications |
EASA_and_FAA_certified
|
| gptkbp:community |
active support forums and resources
|
| gptkbp:compressionRatio |
9.5:1
|
| gptkbp:controls |
electric starter
|
| gptkbp:coolingSystem |
liquid-cooled
air-cooled and liquid-cooled options |
| gptkbp:cylinderCount |
4
flat-four |
| gptkbp:displacement |
100 hp
|
| gptkbp:drivetrain |
SOHC
|
| gptkbp:engine |
modular design
approximately 600 mm compact and lightweight approximately 500 mm approximately 400 mm silver or black |
| gptkbp:engineConfiguration |
horizontally opposed
|
| gptkbp:engineType |
reliable and efficient operation
|
| gptkbp:exhaustSystem |
dual exhaust
|
| gptkbp:fuel_capacity |
approximately 3.5 L
approximately 5.5 to 7.5 L/h |
| gptkbp:fuelType |
aviation gasoline
dual ignition carbureted or fuel injected NGK or equivalent |
| gptkbp:hasArea |
bench tested before delivery
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rotax 912 engine
|
| gptkbp:introduced |
1989
|
| gptkbp:maintenance |
100 hours
|
| gptkbp:manufacturer |
gptkb:BRP-Rotax
|
| gptkbp:market_segment |
general aviation
|
| gptkbp:maximum_speed |
5500 RPM
|
| gptkbp:notable_feature |
912 ULS, 912 S, 912 iS
|
| gptkbp:notableUsers |
Pipistrel,_Tecnam
|
| gptkbp:operationalHistory |
evolved_from_earlier_Rotax_models.
|
| gptkbp:performances |
high power-to-weight ratio
approximately 2000 hours widely used in ultralight aircraft |
| gptkbp:powerOutput |
80 to 100 hp
|
| gptkbp:propulsion |
constant speed propeller
|
| gptkbp:related_engine |
alternator, starter motor
|
| gptkbp:torque |
max torque of 100 Nm
|
| gptkbp:type |
four-stroke engine
|
| gptkbp:updates |
available for improved performance
|
| gptkbp:warranty |
2 years or 1000 hours
|
| gptkbp:weight |
approximately 60 kg
|