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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:aircraft_configuration
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gptkb:Beechcraft_Baron
gptkb:Piper_Navajo
gptkb:Mooney_M20
gptkb:Cessna_210
gptkb:Grumman_American_AA-5
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gptkbp:application
|
General aviation aircraft
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gptkbp:ceo
|
1,700 hours
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gptkbp:compression_ratio
|
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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Throttle control
Electronic ignition
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gptkbp:cooling_system
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Air-cooled
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gptkbp:displacement
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520 cubic inches
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gptkbp:engine
|
Electric start
Long history in aviation
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gptkbp:engine_configuration
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Inline
Engine mount type
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gptkbp:engine_power
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High reliability
High performance
Widely used in general aviation.
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gptkbp:engine_type
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Turbocharged
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gptkbp:exhaust_system
|
Dual exhaust
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gptkbp:first_introduced
|
1960s
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gptkbp:fuel_capacity
|
12 quarts
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gptkbp:fuel_type
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gptkb:Avgas
Fuel injection
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Continental TSIO-520-U
|
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gptkbp:ignition_system
|
gptkb:Champion_REM40_E
Dual ignition
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|
gptkbp:maintenance
|
Regular maintenance required
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gptkbp:manufacturer
|
gptkb:Continental_Motors
|
|
gptkbp:max_speed
|
2,700 RPM
|
|
gptkbp:noise_level
|
Low vibration
Moderate noise
|
|
gptkbp:powers
|
300 horsepower
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gptkbp:propeller
|
Constant speed propeller
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|
gptkbp:service_ceiling
|
25,000 feet
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|
gptkbp:torque
|
Wet sump
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|
gptkbp:type
|
Six-cylinder engine
|
|
gptkbp:valve_configuration
|
OHV
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gptkbp:warranty
|
Limited warranty available
|
|
gptkbp:water_requirement
|
20-30 gallons per hour
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gptkbp:weight
|
approximately 300 lbs
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gptkbp:bfsParent
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gptkb:Cessna_340
gptkb:Cessna_421
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gptkbp:bfsLayer
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6
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