|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
general aviation aircraft
|
|
gptkbp:bore
|
5.125 inches
|
|
gptkbp:ceo
|
1800 hours
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:color
|
gray
|
|
gptkbp:compression_ratio
|
8.5:1
|
|
gptkbp:configuration
|
horizontally opposed
|
|
gptkbp:control_system
|
mechanical throttle
|
|
gptkbp:cooling_fins
|
present
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:displacement
|
540 cubic inches
|
|
gptkbp:engine
|
gptkb:Lycoming_IO-540
gptkb:Lycoming_O-540
four-stroke
Lycoming O series
|
|
gptkbp:engine_configuration
|
flat engine
V-type engine
|
|
gptkbp:engine_type
|
reciprocating engine
VO-540-A
VO-540-B
VO-540-C
VO-540-D
VO-540-E
VO-540-F
VO-540-G
VO-540-H
VO-540-I
VO-540-J
VO-540-K
VO-540-L
VO-540-S
VO-540-U
|
|
gptkbp:first_introduced
|
1960s
|
|
gptkbp:fuel_capacity
|
12 quarts
|
|
gptkbp:fuel_economy
|
12-15 gallons per hour
|
|
gptkbp:fuel_type
|
aviation gasoline
carbureted or fuel injected
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lycoming VO-540
|
|
gptkbp:ignition_system
|
removable
dual ignition
|
|
gptkbp:is_often_used_in
|
fixed-wing aircraft
helicopters
|
|
gptkbp:maintenance
|
100 hours
|
|
gptkbp:manufacturer
|
gptkb:Lycoming_Engines
|
|
gptkbp:market_segment
|
gptkb:light_aircraft
|
|
gptkbp:mounting_options
|
engine mount
|
|
gptkbp:number_of_engines
|
gptkb:6
|
|
gptkbp:power_output
|
250 to 300 horsepower
|
|
gptkbp:propeller
|
constant speed propeller
|
|
gptkbp:related_aircraft
|
gptkb:Beechcraft_Baron
gptkb:Piper_Navajo
gptkb:Cessna_340
|
|
gptkbp:stroke
|
4.00 inches
|
|
gptkbp:type
|
gptkb:V8_engine
|
|
gptkbp:valve_configuration
|
overhead valve
|
|
gptkbp:weight
|
approximately 300 lbs
|
|
gptkbp:bfsParent
|
gptkb:Bell_47_D
gptkb:Bell_47_G
gptkb:Bell_47_J
gptkb:Enstrom_280
|
|
gptkbp:bfsLayer
|
7
|