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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:bore
|
5.125 inches
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|
gptkbp:ceo
|
1,500 hours
|
|
gptkbp:certification
|
FAA certified
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gptkbp:compression_ratio
|
8.5:1 to 10.5:1
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gptkbp:configuration
|
V-type engine
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gptkbp:control_system
|
throttle control
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gptkbp:cooling_system
|
air-cooled
direct air cooling
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gptkbp:displacement
|
540 cubic inches
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gptkbp:engine
|
gptkb:IO-540_family
various accessories available
IO-540 series
long history of use in aviation.
major overhaul required after TBO
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|
gptkbp:engine_configuration
|
inline engine layout
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gptkbp:engine_power
|
high reliability
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gptkbp:engine_type
|
horizontally opposed engine
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|
gptkbp:first_introduced
|
1950s
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gptkbp:fuel_capacity
|
8 quarts
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gptkbp:fuel_type
|
aviation gasoline
carbureted or fuel injected
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming IO-540
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|
gptkbp:ignition_system
|
removable
dual ignition
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|
gptkbp:is_often_used_in
|
gptkb:trainer_aircraft
|
|
gptkbp:maintenance
|
regular maintenance required
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:mounting_options
|
engine mount
|
|
gptkbp:noise_level
|
low vibration
moderate noise level
|
|
gptkbp:notable_applications
|
gptkb:light_aircraft
|
|
gptkbp:number_of_engines
|
gptkb:6
|
|
gptkbp:power_output
|
250 to 300 horsepower
|
|
gptkbp:propeller
|
constant speed propeller
|
|
gptkbp:related_aircraft
|
gptkb:Beechcraft_Bonanza
gptkb:Grumman_AA-5
gptkb:Mooney_M20
gptkb:Cessna_182
gptkb:Piper_PA-28_R
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|
gptkbp:stroke
|
4.00 inches
|
|
gptkbp:type
|
four-stroke engine
|
|
gptkbp:used_in
|
general aviation aircraft
|
|
gptkbp:valve_configuration
|
overhead valve
|
|
gptkbp:variant
|
IO-540-U2 A5
|
|
gptkbp:weight
|
approximately 300 lbs
|
|
gptkbp:bfsParent
|
gptkb:Textron
gptkb:Robinson
|
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gptkbp:bfsLayer
|
5
|