IO-540 engine

GPTKB entity

Statements (55)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 4
gptkbp:bfsParent gptkb:Lycoming_Engines
gptkbp:application gptkb:Piper_PA-32
gptkb:Beechcraft_Bonanza
gptkb:Cessna_182
gptkbp:bore 5.125 inches
gptkbp:ceo 1800 hours
gptkbp:compression_ratio 8.5:1
gptkbp:controls throttle control
gptkbp:cooling_system air-cooled
finned cylinders
gptkbp:displacement 540 cubic inches
gptkbp:emissions_standard dual intake manifold
exhaust stacks
gptkbp:engine gptkb:Company
gptkb:Pokémon
gptkb:engine
aluminum alloy
high reliability
inline engine
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 mount system
engine analyzer
gptkbp:engine_type IO-550 engine
horizontally opposed engine
roller camshaft
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 dual ignition
Champion RE M40 E
gptkbp:maintenance 100 hours
gptkbp:manufacturer gptkb:Teledyne_Continental_Motors
gptkbp:max_speed 2700 RPM
gptkbp:power_output 300 horsepower
gptkbp:propulsion constant speed propeller
gptkbp:setting six-cylinder
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