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gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:ceo
|
1,500 hours
|
|
gptkbp:compression_ratio
|
8.5:1 to 10:1
|
|
gptkbp:configuration
|
6-cylinder
|
|
gptkbp:control_system
|
throttle and mixture control
|
|
gptkbp:cooling_fins
|
integrated cooling fins
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:displacement
|
540 cubic inches
|
|
gptkbp:engine
|
major overhaul required every 1,500 hours
Lycoming IO-540 family
|
|
gptkbp:engine_configuration
|
inline engine
front-mounted
|
|
gptkbp:engine_power
|
up to 2,000 hours with proper maintenance
|
|
gptkbp:engine_type
|
reciprocating engine
gear-driven camshaft
AEIO-540-K1 A5
AEIO-540-L1 A5
AEIO-540-L2 A
AEIO-540-U
AEIO-540-U1 A5
|
|
gptkbp:exhaust_system
|
dual exhaust
|
|
gptkbp:first_introduced
|
1960s
|
|
gptkbp:fuel_capacity
|
12 quarts
|
|
gptkbp:fuel_type
|
aviation gasoline
carbureted or fuel injected
aviation grade oil
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming AEIO-540
|
|
gptkbp:ignition_system
|
gptkb:Champion_REM40_E
dual ignition
|
|
gptkbp:is_tested_for
|
bench testing required
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:market_segment
|
general aviation
|
|
gptkbp:modifications
|
turbocharging
propeller upgrades
fuel injection conversion
|
|
gptkbp:notable_applications
|
gptkb:Piper_PA-32
gptkb:Beechcraft_Bonanza
gptkb:Cessna_182
|
|
gptkbp:number_of_engines
|
aluminum alloy
|
|
gptkbp:power_output
|
250 to 300 horsepower
|
|
gptkbp:propeller
|
constant speed propeller
|
|
gptkbp:propulsion
|
0.83 hp/lb
|
|
gptkbp:regulatory_compliance
|
FAA certified
|
|
gptkbp:service_ceiling
|
15,000 feet
|
|
gptkbp:type
|
horizontally opposed engine
|
|
gptkbp:used_in
|
general aviation aircraft
|
|
gptkbp:valve_configuration
|
overhead valve
|
|
gptkbp:water_requirement
|
up to 30 gallons per hour
|
|
gptkbp:weight
|
approximately 300 lbs
|
|
gptkbp:bfsParent
|
gptkb:Aviat_Super_Decathlon
|
|
gptkbp:bfsLayer
|
6
|