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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compression_ratio
|
8.5:1
|
|
gptkbp:configuration
|
horizontally opposed
|
|
gptkbp:control_system
|
throttle and mixture control
|
|
gptkbp:cooling_system
|
air-cooled
cylinder head temperature monitoring
|
|
gptkbp:displacement
|
320 cubic inches
|
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gptkbp:engine
|
gptkb:O-320_series
requires specialized knowledge
|
|
gptkbp:engine_configuration
|
inline engine
front-mounted
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|
gptkbp:engine_power
|
reliable and efficient
|
|
gptkbp:engine_type
|
gptkb:O-320-A1_A
gptkb:O-320-D2_A
gptkb:O-320-E2_A
gptkb:O-320-F2_A
gptkb:O-320-H2_AD
gptkb:O-320-J2_A
gptkb:O-320-U2_A
reciprocating engine
O-320-B1 A
O-320-C1 A
O-320-L2 A
|
|
gptkbp:first_introduced
|
1953
|
|
gptkbp:fuel_capacity
|
8 quarts
|
|
gptkbp:fuel_type
|
aviation gasoline
carbureted or fuel-injected
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming O-320
|
|
gptkbp:ignition_system
|
removable
dual ignition
|
|
gptkbp:is_tested_for
|
bench testing required
|
|
gptkbp:maintenance
|
regular oil changes
valve adjustments
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:max_speed
|
2,700 RPM
|
|
gptkbp:modifications
|
increased horsepower
upgraded fuel injection
|
|
gptkbp:notable_applications
|
gptkb:light_aircraft
|
|
gptkbp:notable_models
|
gptkb:Boeing_707
gptkb:Mooney_M20
Piper PA-28
|
|
gptkbp:number_of_engines
|
four
|
|
gptkbp:power_output
|
150 to 160 horsepower
|
|
gptkbp:propeller
|
fixed-pitch or constant-speed
|
|
gptkbp:tbo_(time_between_overhaul)
|
1,500 hours
|
|
gptkbp:type
|
four-cylinder engine
|
|
gptkbp:used_in
|
general aviation aircraft
|
|
gptkbp:valve_configuration
|
OHV (overhead valve)
|
|
gptkbp:weight
|
approximately 300 pounds
|
|
gptkbp:bfsParent
|
gptkb:Cessna_172_F
gptkb:Cessna_172_J
gptkb:Cessna_172_L
gptkb:Cessna_172_M
|
|
gptkbp:bfsLayer
|
5
|