IO-540 engine

GPTKB entity

Statements (56)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:bore 5.125 inches
gptkbp:ceo 1800 hours
gptkbp:compression_ratio 8.5:1
gptkbp:configuration six-cylinder
gptkbp:control_system throttle control
gptkbp:cooling_system air-cooled
finned cylinders
gptkbp:displacement 540 cubic inches
gptkbp:engine gptkb:Twix
gptkb:gasoline
gptkb:electric_vehicles
magnetos
tachometer
starter motor
oil temperature gauge
fuel pressure gauge
engine monitor system
manifold pressure gauge
prop governor
widely used in light aircraft
cylinder head temperature gauge
engine analyzer
gptkbp:engine_configuration inline engine
engine mount system
gptkbp:engine_power high reliability
gptkbp:engine_type IO-550 engine
horizontally opposed engine
roller camshaft
gptkbp:exhaust_system dual intake manifold
exhaust stacks
gptkbp:first_introduced 1950s
gptkbp:fuel_capacity 8 quarts
gptkbp:fuel_type aviation gasoline
carbureted
optional fuel injection
https://www.w3.org/2000/01/rdf-schema#label IO-540 engine
gptkbp:ignition_system gptkb:Champion_REM40_E
dual ignition
gptkbp:maintenance 100 hours
gptkbp:manufacturer gptkb:Teledyne_Continental_Motors
gptkbp:max_speed 2700 RPM
gptkbp:notable_applications gptkb:Piper_PA-32
gptkb:Beechcraft_Bonanza
gptkb:Cessna_182
gptkbp:number_of_engines aluminum alloy
gptkbp:power_output 300 horsepower
gptkbp:propeller constant speed propeller
gptkbp:stroke 4.0 inches
gptkbp:type reciprocating engine
gptkbp:used_in general aviation aircraft
gptkbp:valve_configuration overhead valve
gptkbp:weight approximately 360 lbs
gptkbp:bfsParent gptkb:Lycoming
gptkb:Lycoming_Engines
gptkbp:bfsLayer 6