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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:turbofan_engine
gptkb:Pistons
Alternator
Fuel pump
Air filter
Engine instruments
Intake manifold
Fuel injectors
Magnetos
Mounting brackets
Oil cooler
Cooling baffles
Starter motor
Ignition harness
Oil filter
Connecting rods
Fuel lines
Cylinder heads
Exhaust pipes
Prop governor
Throttle linkage
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gptkbp:application
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gptkb:Beechcraft_Bonanza
gptkb:Piper_Navajo
gptkb:Mooney_M20
gptkb:Cessna_210
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gptkbp:bore
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5.125 inches
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gptkbp:ceo
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1,700 hours
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gptkbp:certification
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FAA certified
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gptkbp:compression_ratio
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8.5:1
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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
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gptkbp:cooling_system
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Air-cooled
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gptkbp:displacement
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520 cubic inches
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gptkbp:engine
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gptkb:Continental_IO-550
gptkb:Continental_IO-360
gptkb:Continental_TSIO-520
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gptkbp:engine_configuration
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Engine mount type
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gptkbp:engine_type
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Reciprocating engine
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gptkbp:exhaust_system
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Exhaust stacks
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gptkbp:first_introduced
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1950s
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gptkbp:fuel_capacity
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Wet sump
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gptkbp:fuel_type
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gptkb:Avgas
Fuel injection
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https://www.w3.org/2000/01/rdf-schema#label
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Continental IO-520
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gptkbp:ignition_system
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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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285 to 300 horsepower
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gptkbp:propeller
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Constant speed propeller
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gptkbp:stroke
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4.75 inches
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gptkbp:type
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Six-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 valve
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gptkbp:weight
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Approx. 300 lbs
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gptkbp:bfsParent
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gptkb:Beechcraft_35-C33_Debonair
gptkb:Cessna_310
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gptkbp:bfsLayer
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6
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