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gptkbp:instanceOf
|
gptkb:aircraft_engine_family
|
|
gptkbp:application
|
gptkb:aircraft
gptkb:trainer_aircraft
general aviation
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compressionRatio
|
7.00:1
8.50:1
|
|
gptkbp:configuration
|
naturally aspirated
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:displacement
|
320 cubic inches
|
|
gptkbp:engineType
|
horizontally opposed
four-cylinder
|
|
gptkbp:firstFlight
|
1953
|
|
gptkbp:fuelType
|
aviation gasoline
carbureted
fuel injected
|
|
gptkbp:governingBody
|
gptkb:Federal_Aviation_Administration
|
|
gptkbp:ignition
|
dual magneto
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:notableVariant
|
gptkb:O-320-A
gptkb:O-320-B
gptkb:O-320-D
gptkb:O-320-E
gptkb:O-320-H
gptkb:O-320-X
O-320-F
O-320-L
O-320-R
O-320-T
O-320-U
O-320-W
|
|
gptkbp:numberOfEngines
|
5.125 inches
|
|
gptkbp:pistonStroke
|
3.875 inches
|
|
gptkbp:powerOutput
|
150 hp
160 hp
|
|
gptkbp:relatedTo
|
gptkb:Lycoming_O-360_family
Lycoming O-235 family
|
|
gptkbp:successor
|
gptkb:Lycoming_O-360_family
|
|
gptkbp:usedIn
|
gptkb:Cessna_172
gptkb:Grumman_American_AA-5
gptkb:Piper_Cherokee
gptkb:Piper_PA-18_Super_Cub
gptkb:Beechcraft_Musketeer
|
|
gptkbp:valveConfiguration
|
overhead valve
|
|
gptkbp:weight
|
244 lbs
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_O-360_family
|
|
gptkbp:bfsLayer
|
8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming O-320 family
|