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gptkbp:instance_of
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gptkb:engine
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gptkbp:aircraft_operated
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gptkb:Piper_Seminole
gptkb:aircraft
gptkb:Cessna_177
gptkb:Beechcraft_Bonanza
gptkb:Piper_Navajo
gptkb:Grumman_AA-5
gptkb:Mooney_M20
gptkb:Cessna_185
gptkb:Cessna_210
gptkb:Cessna_150
gptkb:Piper_Comanche
gptkb:Piper_Aztec
gptkb:Piper_Arrow
gptkb:Piper_Warrior
gptkb:Piper_Archer
gptkb:Cessna_182
gptkb:Cessna_172_RG
gptkb:Cessna_177_RG
Piper PA-28
Diamond D A40
Cirrus S R20
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gptkbp:application
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general aviation aircraft
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gptkbp:bore
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5.0 inches
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gptkbp:ceo
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1800 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:controls
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gptkb:book
throttle
propeller pitch
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gptkbp:cooling_system
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air-cooled
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gptkbp:displacement
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360 cubic inches
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gptkbp:engine
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gptkb:4
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gptkbp:first_flight
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1960s
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gptkbp:fuel_capacity
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wet sump
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gptkbp:fuel_type
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aviation gasoline
gravity fed
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https://www.w3.org/2000/01/rdf-schema#label
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IO-360-MB
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gptkbp:ignition_system
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dual ignition
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gptkbp:launch_site
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electric starter
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gptkbp:maintenance
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100 hours
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gptkbp:manufacturer
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gptkb:Lycoming
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gptkbp:power_output
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180 horsepower
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gptkbp:propulsion
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constant speed
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gptkbp:related_model
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gptkb:IO-360-L2_A
O-360
IO-360-B1 A
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gptkbp:setting
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horizontally opposed
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gptkbp:stroke
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4.0 inches
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gptkbp:type
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four-stroke
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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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