|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:aerobaticVariant
|
AEIO-540
|
|
gptkbp:application
|
gptkb:aircraft
general aviation
helicopters
|
|
gptkbp:bore
|
5.125 in
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compressionRatio
|
8.5:1
|
|
gptkbp:configuration
|
horizontally opposed
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:displacement
|
541.5 cubic inches
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:family
|
gptkb:Lycoming_O-360_family
|
|
gptkbp:firstFlight
|
1957
|
|
gptkbp:fuelType
|
aviation gasoline
carbureted
fuel injected
|
|
gptkbp:helicopterVariant
|
HIO-540
VO-540
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming O-540
|
|
gptkbp:ignition
|
dual magnetos
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:notableFeature
|
widely used in general aviation
|
|
gptkbp:numberOfEngines
|
6
|
|
gptkbp:powerOutput
|
235 to 350 hp
|
|
gptkbp:stroke
|
4.375 in
|
|
gptkbp:superchargedVariant
|
IGSO-540
|
|
gptkbp:turbochargedVariant
|
TIO-540
|
|
gptkbp:usedIn
|
gptkb:Bell_206L_LongRanger
gptkb:Cessna_182
gptkb:Piper_PA-23_Aztec
gptkb:Piper_PA-28_Cherokee
gptkb:Piper_PA-32_Cherokee_Six
gptkb:Robinson_R44
gptkb:Rockwell_Commander_114
gptkb:Piper_PA-24_Comanche
|
|
gptkbp:valvetrain
|
overhead valve
|
|
gptkbp:variant
|
AEIO-540
HIO-540
IGO-540
IGSO-540
IO-540
TIO-540
TIO-541
TVO-540
VO-540
|
|
gptkbp:weight
|
approx 380-440 lbs
|
|
gptkbp:bfsParent
|
gptkb:Maule_M7-260C
gptkb:Piper_PA-32
gptkb:SOCATA_TB_30_Epsilon
gptkb:Socata_TB-30_Epsilon
gptkb:Rutan_Model_72_Grizzly
gptkb:Aermacchi_SF-260
gptkb:Epsilon_TB-30
gptkb:Piper_PA-32_Cherokee_Six
gptkb:Robinson_R44
gptkb:TB_30_Epsilon
gptkb:Aermacchi_SF.260
gptkb:Piper_PA-25
gptkb:Piper_PA-75
gptkb:Piper_PA-95
gptkb:SF.260
gptkb:SOCATA_TB-30_Epsilon
gptkb:SOCATA_TB-30_Epsilon_GT
gptkb:SOCATA_TB-30_Epsilon_Pro
gptkb:SOCATA_TB-30_Epsilon_XL
gptkb:SIAI-Marchetti_SF.260W
|
|
gptkbp:bfsLayer
|
6
|