|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:application
|
general aviation
|
|
gptkbp:bore
|
5.125 in
|
|
gptkbp:category
|
piston aircraft engine
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compressionRatio
|
8.5:1
|
|
gptkbp:configuration
|
flat-four
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:displacement
|
361 cubic inches
|
|
gptkbp:engineType
|
horizontally opposed
four-cylinder
|
|
gptkbp:family
|
gptkb:Lycoming_O-360_family
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:fuelType
|
avgas
approx 9-10 gph at cruise
carbureted
fuel injected
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Textron Lycoming O-360
|
|
gptkbp:ignition
|
dual magnetos
|
|
gptkbp:manufacturer
|
gptkb:Textron
gptkb:Lycoming_Engines
|
|
gptkbp:marketedAs
|
gptkb:Lycoming_Engines
|
|
gptkbp:notableFor
|
widespread use in light aircraft
|
|
gptkbp:notableVariant
|
gptkb:O-360-A1A
gptkb:O-360-A4M
gptkb:O-360-C1G6D
|
|
gptkbp:numberOfEngines
|
4
|
|
gptkbp:oilSystem
|
wet sump
|
|
gptkbp:powerOutput
|
180 hp
|
|
gptkbp:predecessor
|
gptkb:Lycoming_O-320
|
|
gptkbp:primaryUse
|
single-engine aircraft
|
|
gptkbp:propulsion
|
direct drive
|
|
gptkbp:rpm
|
2700 max continuous
|
|
gptkbp:stroke
|
4.375 in
|
|
gptkbp:successor
|
gptkb:Lycoming_IO-360
|
|
gptkbp:usedIn
|
gptkb:Diamond_DA40
gptkb:Mooney_M20
gptkb:Piper_Cherokee
gptkb:Beechcraft_Musketeer
Cessna 172
|
|
gptkbp:valvesPerCylinder
|
2
|
|
gptkbp:valvetrain
|
overhead valve
|
|
gptkbp:variant
|
gptkb:O-360-A1A
gptkb:O-360-A4M
gptkb:O-360-C1G6D
|
|
gptkbp:weight
|
approx 285 lbs
|
|
gptkbp:bfsParent
|
gptkb:Grob_Tutor_T1
|
|
gptkbp:bfsLayer
|
6
|