Continental O-190-1

GPTKB entity

Statements (42)
Predicate Object
gptkbp:instanceOf Aircraft engine
gptkbp:application gptkb:Piper_PA-22_Tri-Pacer
gptkb:Cessna_150
Aeronca Champ
gptkbp:bore 4.0 inches
gptkbp:compressionRatio 7.0:1
gptkbp:controls Mixture
Throttle
Propeller_pitch
gptkbp:coolingSystem Air-cooled
Air cooling
gptkbp:cylinderCount 4
gptkbp:displacement 190 cubic inches
gptkbp:drivetrain Overhead valve
gptkbp:engine Front-mounted
Designed for general aviation.
Horizontally_opposed_layout
gptkbp:engineConfiguration Inline
gptkbp:engineType Four-stroke
gptkbp:fuel_capacity 6 quarts
10 gallons per hour
gptkbp:fuelType Magneto
Champion
Avgas
https://www.w3.org/2000/01/rdf-schema#label Continental O-190-1
gptkbp:introduced 1950s
gptkbp:is_used_in General aviation aircraft
gptkbp:manufacturer gptkb:Continental_Motors
gptkbp:mayHave 1800 hours
gptkbp:operationalHistory Used in various light aircraft
gptkbp:performances Regular maintenance required
Reliable performance
gptkbp:powerOutput 95 horsepower
gptkbp:propulsion Fixed-pitch
gptkbp:related_engine gptkb:O-190_series
gptkb:Continental_O-200
gptkb:Continental_O-300
gptkbp:setting Horizontally_opposed
gptkbp:stroke 4.0 inches
gptkbp:torque Wet sump
gptkbp:type Reciprocating engine
gptkbp:weight approximately 250 lbs