|
gptkbp:instanceOf
|
gptkb:aircraft_engine_family
|
|
gptkbp:bore
|
5.125 inches
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compressionRatio
|
8.50:1
8.70:1
9.00:1
|
|
gptkbp:configuration
|
horizontally opposed
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:displacement
|
360 cubic inches
|
|
gptkbp:fuelType
|
100LL avgas
fuel injected
|
|
gptkbp:ignition
|
dual magnetos
|
|
gptkbp:introducedIn
|
1965
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:marketedAs
|
gptkb:Lycoming_IO-360
|
|
gptkbp:notableVariant
|
gptkb:AIO-360
gptkb:HIO-360
gptkb:IO-360-A1A
gptkb:IO-360-L2A
gptkb:LIO-360
IO-360-B1A
IO-360-C1C
TIO-360
|
|
gptkbp:numberOfEngines
|
4
|
|
gptkbp:oil_system
|
wet sump
|
|
gptkbp:powerOutput
|
180 to 200 horsepower
|
|
gptkbp:primaryUse
|
general aviation aircraft
|
|
gptkbp:propeller_drive
|
direct drive
|
|
gptkbp:stroke
|
4.375 inches
|
|
gptkbp:usedInAircraft
|
gptkb:Diamond_DA40
gptkb:Grumman_Tiger
gptkb:Mooney_M20J
gptkb:Socata_TB-20_Trinidad
gptkb:Rockwell_Commander_112
gptkb:Beechcraft_Musketeer
gptkb:Piper_Arrow
gptkb:Cessna_172S
|
|
gptkbp:valve_train
|
overhead valve
|
|
gptkbp:weight_(dry)
|
approx. 285 lbs
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_IO-360
|
|
gptkbp:bfsLayer
|
8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
IO-360 Series
|