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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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gptkb:Boeing_707
gptkb:Beechcraft_Bonanza
gptkb:Mooney_M20
gptkb:Grumman_American_AA-5
Piper PA-28
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gptkbp:compression_ratio
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8.5:1 to 9.0:1
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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:battery
gptkb:carburetor
gptkb:gasoline
gptkb:electric_vehicles
gptkb:regulations
engine control unit
magnetos
tachometer
1200 hours
starter motor
oil temperature gauge
fuel pressure gauge
circuit breaker panel
manifold pressure gauge
prop governor
RPM gauge
fuel selector valve
cylinder head temperature gauge
engine monitor
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gptkbp:engine_configuration
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inline engine
front-mounted
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gptkbp:engine_power
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2000 hours
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gptkbp:engine_type
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reciprocating engine
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gptkbp:exhaust_system
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dual exhaust
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gptkbp:first_introduced
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1950s
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gptkbp:fuel_capacity
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8 quarts
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gptkbp:fuel_economy
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12 to 15 gallons per hour
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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 O-540 family
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gptkbp:ignition_system
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gptkb:Champion_REM40_E
dual ignition
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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:number_of_engines
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horizontally opposed
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gptkbp:power_output
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250 to 300 horsepower
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gptkbp:propeller
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constant speed propeller
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gptkbp:service_ceiling
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15,000 feet
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gptkbp:torque
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wet sump
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gptkbp:tuning
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fixed pitch propeller
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gptkbp:type
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four-cylinder engine
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gptkbp:used_in
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general aviation aircraft
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gptkbp:valve_configuration
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overhead valve
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gptkbp:variant
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O-540-U2 A
O-540-E4 B5
O-540-L2 A5
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gptkbp:weight
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approximately 300 pounds
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gptkbp:bfsParent
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gptkb:Lycoming_TIO-540-U2_A
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gptkbp:bfsLayer
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7
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