|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Piper_J-3_Cub
|
|
gptkbp:aircraft_operated
|
gptkb:Cessna_140
gptkb:Piper_J-3_Cub
gptkb:Taylorcraft_BC-12
|
|
gptkbp:application
|
general aviation
|
|
gptkbp:ceo
|
1800 hours
|
|
gptkbp:compression_ratio
|
7:1
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:displacement
|
65 cubic inches
|
|
gptkbp:engine
|
gptkb:4
gptkb:Continental_O-200
inline-four
horizontally opposed
front-mounted
|
|
gptkbp:engine_type
|
four-stroke engine
|
|
gptkbp:first_flight
|
1946
|
|
gptkbp:fuel_capacity
|
68 kg
24 inches
22 inches
30 inches
6 quarts
|
|
gptkbp:fuel_type
|
aviation gasoline
carbureted
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Continental A-65
|
|
gptkbp:ignition_system
|
gptkb:Champion_REM-40
magneto ignition
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
gptkb:Continental_Motors
|
|
gptkbp:operational_range
|
2000-2800 RPM
|
|
gptkbp:power_output
|
65 horsepower
|
|
gptkbp:production_years
|
1946-1955
|
|
gptkbp:propulsion
|
fixed-pitch
|
|
gptkbp:setting
|
inline engine
|
|
gptkbp:successor
|
gptkb:Continental_A-75
|
|
gptkbp:type
|
reciprocating engine
|
|
gptkbp:used_in
|
gptkb:aircraft
|
|
gptkbp:valve_configuration
|
overhead valves
|
|
gptkbp:weight
|
approximately 150 pounds
|