O-320-U2 A

GPTKB entity

Statements (58)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:application gptkb:aircraft
gptkb:Mooney_M20
gptkb:Beechcraft_Musketeer
Piper PA-28
gptkbp:compression_ratio 8.5:1
gptkbp:controls constant speed propeller
manual throttle control
mechanical control system
gptkbp:cooling_system air-cooled
air cooling system
no cooling fan required
gptkbp:displacement 320 cubic inches
gptkbp:emissions_standard exhaust system included
gptkbp:enforces FAA certified
gptkbp:engine gptkb:O-320_series
electric starter
inline
reliable performance
various accessories available
horizontally opposed
detailed specifications available
mounting brackets included
widely used in training aircraft
long history in aviation
compatible with various propellers
performance data available
2000 hours TBO
engine mount type
intake manifold included
gptkbp:engine_type reciprocating engine
multiple variants exist
gptkbp:first_introduced 1950s
gptkbp:fuel_capacity 10-12 gallons per hour
compatible with standard fuel tanks
gptkbp:fuel_type aviation gasoline
carbureted or fuel injected
mechanical fuel pump
https://www.w3.org/2000/01/rdf-schema#label O-320-U2 A
gptkbp:ignition_system dual ignition
magneto ignition system
gptkbp:is_tested_for bench tested
gptkbp:maintenance regular maintenance required
gptkbp:manufacturer gptkb:Lycoming
gptkbp:noise_level low vibration
moderate noise level
gptkbp:power_output 150 horsepower
gptkbp:propulsion fixed-pitch or constant-speed
gptkbp:service_ceiling 15,000 feet
gptkbp:setting horizontally opposed
gptkbp:torque wet sump system
gptkbp:type four-cylinder
gptkbp:used_in general aviation aircraft
gptkbp:valve_configuration OHV
gptkbp:warranty limited warranty available
gptkbp:weight approximately 300 pounds
gptkbp:bfsParent gptkb:Lycoming_O-320
gptkbp:bfsLayer 5