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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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general aviation aircraft
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gptkbp:certification
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FAA certified
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gptkbp:compression_ratio
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8.5:1
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gptkbp:configuration
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horizontally opposed
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gptkbp:control_system
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mechanical throttle
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gptkbp:cooling_system
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air-cooled
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gptkbp:displacement
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540 cubic inches
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gptkbp:engine
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gptkb:Piper_Seminole
gptkb:turbofan_engine
gptkb:Boeing_707
gptkb:Beechcraft_Baron
gptkb:Cessna_182_T
gptkb:Lycoming_O-540_family
gptkb:Mooney_M20_V
gptkb:TIO_series
gptkb:Piper_Navajo
gptkb:Piper_Cherokee_6
gptkb:Cessna_210
gptkb:Piper_Aztec
gptkb:Piper_Arrow
gptkb:Cessna_172_RG
four-stroke
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gptkbp:engine_configuration
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inline engine
250 HP at 2700 RPM
TIO-540-U2 A
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gptkbp:engine_displacement
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8.8 liters
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gptkbp:engine_type
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turbocharged engine
TIO-540
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gptkbp:exhaust_system
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dual exhaust
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gptkbp:first_introduced
|
1960s
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gptkbp:fuel_capacity
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12 quarts
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gptkbp:fuel_type
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aviation gasoline
carbureted
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|
https://www.w3.org/2000/01/rdf-schema#label
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Lycoming TIO-540-U2 A
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gptkbp:ignition_system
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dual ignition
REM40 E
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gptkbp:is_often_used_in
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used in various aircraft models
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gptkbp:maintenance
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100 hours
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gptkbp:manufacturer
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gptkb:Lycoming_Engines
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gptkbp:mounting_options
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engine mount
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gptkbp:power_output
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250 horsepower
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gptkbp:propeller
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constant speed propeller
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gptkbp:tuning
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factory tuned
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gptkbp:type
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six-cylinder engine
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gptkbp:valve_configuration
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overhead valve
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gptkbp:water_requirement
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15-20 gallons per hour
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gptkbp:weight
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approximately 300 lbs
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gptkbp:bfsParent
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gptkb:Piper_Aerostar
gptkb:Piper_Aerostar_600
gptkb:Piper_PA-31-350_Chieftain
gptkb:Piper_PA-46-350_P_Malibu_Mirage
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gptkbp:bfsLayer
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6
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