Continental O-200

GPTKB entity

Statements (58)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:aircraft_operated gptkb:Mooney_M20
gptkb:Piper_PA-18_Super_Cub
gptkb:Cessna_150
gptkb:Beechcraft_Musketeer
gptkbp:bore 3.5 inches
gptkbp:ceo 1,500 hours
gptkbp:compression_ratio 8.5:1
gptkbp:configuration horizontally opposed
gptkbp:control_system throttle control
mixture control
propeller control
gptkbp:cooling_system air-cooled
gptkbp:displacement 200 cubic inches
gptkbp:engine electric starter
manual start option
gptkbp:engine_configuration inline
front-mounted
gptkbp:engine_power smooth operation
good climb rate
low vibration
reliable starting
good fuel efficiency
gptkbp:engine_type reciprocating engine
gptkbp:first_flight 1950s
gptkbp:fuel_capacity 6 quarts
gptkbp:fuel_economy approximately 8-10 gallons per hour
gptkbp:fuel_type aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label Continental O-200
gptkbp:ignition_system gptkb:Champion_REM40
dual ignition
gptkbp:maintenance regular inspections required
carburetor overhaul required every 1,000 hours
oil changes required every 50 hours
spark plug replacement required every 100 hours
valve adjustments required every 500 hours
gptkbp:manufacturer gptkb:Continental_Motors
gptkbp:notable_applications gptkb:trainer_aircraft
aerial photography
recreational flying
agricultural aviation
glider towing
gptkbp:power_output 100 horsepower
gptkbp:propeller fixed-pitch or constant-speed
gptkbp:service_ceiling approximately 12,000 feet
gptkbp:stroke 4 inches
gptkbp:type four-cylinder engine
gptkbp:used_in gptkb:light_aircraft
gptkbp:valve_configuration overhead valves
gptkbp:weight approximately 240 pounds
gptkbp:bfsParent gptkb:Piper_J-3_C-140
gptkb:Piper_J-3_C-250
gptkb:Piper_J-3_C-260
gptkb:Continental_A-65
gptkb:Cessna_162
gptkb:Caproni_Ca.300
gptkb:Cessna_150_L
gptkbp:bfsLayer 6