|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:application
|
general aviation aircraft
|
|
gptkbp:bore
|
5.125 inches
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compressionRatio
|
8.50:1
|
|
gptkbp:configuration
|
horizontally opposed
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:cycle
|
four-stroke
|
|
gptkbp:displacement
|
360 cubic inches
|
|
gptkbp:engineType
|
four-cylinder
|
|
gptkbp:family
|
gptkb:Lycoming_O-360_family
|
|
gptkbp:firstFlight
|
1960s
|
|
gptkbp:fuelType
|
100LL avgas
fuel injected
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming IO-360
|
|
gptkbp:ignition
|
dual magnetos
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:marketedAs
|
gptkb:IO-360_Series
|
|
gptkbp:notableFeature
|
fuel injection for improved altitude performance
|
|
gptkbp:notableVariant
|
gptkb:IO-360-A1A
gptkb:IO-360-B1F
gptkb:IO-360-C1C6
gptkb:IO-360-L2A
gptkb:IO-360-M1A
|
|
gptkbp:numberOfEngines
|
4
|
|
gptkbp:oilSystem
|
wet sump
|
|
gptkbp:powerOutput
|
180 to 200 horsepower
|
|
gptkbp:propulsion
|
direct drive
|
|
gptkbp:range
|
up to 2700 rpm
|
|
gptkbp:relatedTo
|
gptkb:Lycoming_O-360
gptkb:Lycoming_AEIO-360
gptkb:Lycoming_TIO-360
gptkb:Lycoming_LIO-360
|
|
gptkbp:stroke
|
4.375 inches
|
|
gptkbp:usedIn
|
gptkb:Diamond_DA40
gptkb:Grumman_Tiger
gptkb:Mooney_M20J
gptkb:Beechcraft_Musketeer
gptkb:Piper_Arrow
gptkb:Cessna_172RG
|
|
gptkbp:valveConfiguration
|
two valves per cylinder
|
|
gptkbp:valvetrain
|
overhead valve
|
|
gptkbp:weight
|
approx 285 lbs
|
|
gptkbp:bfsParent
|
gptkb:Piper_PA-34
gptkb:Beechcraft_Travel_Air
gptkb:Piper_PA-34_Seneca
|
|
gptkbp:bfsLayer
|
6
|