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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:accessories
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gptkb:carburetor
gptkb:gasoline
gptkb:electric_vehicles
oil cooler
starter motor
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gptkbp:application
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gptkb:Piper_PA-22_Tri-Pacer
gptkb:Boeing_707
gptkb:Mooney_M20
gptkb:Beechcraft_Musketeer
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gptkbp:bore
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5.125 inches
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gptkbp:ceo
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1800 hours
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gptkbp:compression_ratio
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7.0:1
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gptkbp:configuration
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horizontally opposed
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gptkbp:control_system
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throttle control
mixture control
propeller control
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gptkbp:cooling_system
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air-cooled
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gptkbp:displacement
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300 cubic inches
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gptkbp:engine
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O-300 series
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gptkbp:engine_configuration
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inline engine
front-mounted
horizontally opposed layout
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gptkbp:engine_power
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smooth operation
high reliability
easy maintenance
long service life
good power-to-weight ratio
low vibration
good fuel efficiency
suitable for recreational flying
suitable for training aircraft
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gptkbp:engine_type
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reciprocating engine
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gptkbp:exhaust_system
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dual exhaust
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gptkbp:first_introduced
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1950s
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gptkbp:fuel_capacity
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8 quarts
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gptkbp:fuel_economy
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12-15 gallons per hour
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gptkbp:fuel_type
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aviation gasoline
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https://www.w3.org/2000/01/rdf-schema#label
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Continental O-300
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gptkbp:ignition_system
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gptkb:Champion_REM40
dual ignition
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gptkbp:maintenance
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100 hours
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gptkbp:manufacturer
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gptkb:Continental_Motors
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gptkbp:power_output
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145 horsepower
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gptkbp:propeller
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fixed-pitch or constant-speed
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gptkbp:stroke
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4.0 inches
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gptkbp:type
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four-cylinder engine
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gptkbp:used_in
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general aviation aircraft
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gptkbp:valve_configuration
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overhead valves
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gptkbp:weight
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approximately 300 lbs
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gptkbp:bfsParent
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gptkb:Cessna_172_B
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gptkbp:bfsLayer
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5
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