|
gptkbp:instanceOf
|
gptkb:aircraft_engine_family
|
|
gptkbp:bore
|
5.125 inches
|
|
gptkbp:category
|
piston aircraft engine
|
|
gptkbp:compressionRatio
|
7.3:1 to 8.7:1
|
|
gptkbp:configuration
|
flat-six
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:displacement
|
541.5 cubic inches
|
|
gptkbp:family
|
gptkb:TIO-540-AE2A
gptkb:TIO-540-AH1A
gptkb:TIO-540-J2BD
gptkb:TIO-540-S1AD
|
|
gptkbp:firstFlight
|
1960s
|
|
gptkbp:fuelType
|
aviation gasoline
fuel injected
|
|
gptkbp:induction_system
|
turbocharged
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:numberOfEngines
|
6
|
|
gptkbp:powerOutput
|
250 to 350 horsepower
|
|
gptkbp:relatedTo
|
gptkb:Lycoming_IO-540_series
gptkb:Lycoming_O-540_series
|
|
gptkbp:stroke
|
4.375 inches
|
|
gptkbp:usedInAircraft
|
gptkb:Piper_PA-32R_Saratoga
gptkb:Cessna_404_Titan
gptkb:Piper_Navajo_Chieftain
gptkb:Piper_PA-46_Malibu_Mirage
gptkb:Rockwell_Commander_700
|
|
gptkbp:valve_configuration
|
overhead valve
|
|
gptkbp:weight
|
approximately 500 lbs
|
|
gptkbp:bfsParent
|
gptkb:Lycoming_TIO-540-J2BD
gptkb:Lycoming_TIO-540-F2BD
|
|
gptkbp:bfsLayer
|
7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming TIO-540 series
|