|
gptkbp:instanceOf
|
gptkb:aircraft_engine_family
|
|
gptkbp:bore
|
5.125 inches
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compressionRatio
|
8.5:1
9.0:1
8.7:1
|
|
gptkbp:configuration
|
flat-four
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:cycle
|
four-stroke
|
|
gptkbp:displacement
|
361 cubic inches
|
|
gptkbp:family
|
gptkb:AIO-360
gptkb:HIO-360
gptkb:IO-360-A1A
gptkb:IO-360-L2A
gptkb:LIO-360
AEIO-360
IO-360-B1A
IO-360-C1C
|
|
gptkbp:firstFlight
|
1960s
|
|
gptkbp:fuelType
|
100LL avgas
fuel-injected
|
|
gptkbp:ignition
|
dual magnetos
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:market
|
general aviation
|
|
gptkbp:notableVariant
|
AEIO-360 (aerobatic)
AIO-360 (inverted oil system)
HIO-360 (helicopter)
LIO-360 (left-hand rotation)
|
|
gptkbp:numberOfEngines
|
4
|
|
gptkbp:powerOutput
|
180 to 200 hp
|
|
gptkbp:propulsion
|
direct drive
|
|
gptkbp:relatedTo
|
gptkb:Lycoming_O-360_series
gptkb:Lycoming_IO-540_series
Lycoming IO-320 series
|
|
gptkbp:status
|
in production
|
|
gptkbp:stroke
|
4.375 inches
|
|
gptkbp:usedIn
|
gptkb:Robin_DR400
gptkb:Diamond_DA40
gptkb:Grumman_Tiger
gptkb:Cessna_172RG_Cutlass
gptkb:Mooney_M20J
gptkb:Beechcraft_Musketeer
gptkb:Piper_Arrow
|
|
gptkbp:valvetrain
|
overhead valve
|
|
gptkbp:weight
|
approx 285 lbs
|
|
gptkbp:bfsParent
|
gptkb:PA-34-200_Seneca
gptkb:Lycoming_IO-360-A1B6
|
|
gptkbp:bfsLayer
|
8
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming IO-360 series
|