|
gptkbp:instanceOf
|
aircraft engine family
|
|
gptkbp:bore
|
5.125 in
|
|
gptkbp:category
|
piston aircraft engine
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compressionRatio
|
varies by model
|
|
gptkbp:configuration
|
horizontally opposed
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:cycle
|
four-stroke
|
|
gptkbp:displacement
|
541.5 cubic inches
|
|
gptkbp:family
|
AEIO-540
IGSO-540
IO-540
TIO-540
LTIO-540
TEO-540
|
|
gptkbp:firstFlight
|
1957
|
|
gptkbp:fuelType
|
aviation gasoline
fuel injected
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming IO-540 series
|
|
gptkbp:ignition
|
dual magnetos
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:marketedAs
|
general aviation
|
|
gptkbp:notableFeature
|
reliable and robust design
widely used in light aircraft
multiple turbocharged and aerobatic variants
|
|
gptkbp:notableVariant
|
AEIO-540 (aerobatic)
IGSO-540 (geared, supercharged)
LTIO-540 (left-hand rotation, turbocharged)
TEO-540 (electronic engine management)
TIO-540 (turbocharged)
|
|
gptkbp:numberOfEngines
|
6
|
|
gptkbp:powerOutput
|
235 to 350 hp
|
|
gptkbp:stroke
|
4.375 in
|
|
gptkbp:usedIn
|
gptkb:Cessna_182RG
gptkb:Cessna_206
gptkb:Beechcraft_Baron
gptkb:Piper_PA-32_Cherokee_Six
gptkb:Rockwell_Commander_114
gptkb:Piper_PA-24_Comanche
Piper PA-28R-201T Turbo Arrow IV
|
|
gptkbp:valvetrain
|
overhead valve
|
|
gptkbp:weight
|
approx. 380-440 lbs dry
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_IO-360_series
gptkb:Lycoming_TIO-540_series
|
|
gptkbp:bfsLayer
|
8
|