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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:1976_Formula_Atlantic_Championship
|
|
gptkbp:aircraft_operated
|
gptkb:Chevron_B22
gptkb:Chevron_B26
general aviation
retired
single-engine
personal transport
|
|
gptkbp:category
|
gptkb:aircraft
|
|
gptkbp:certification
|
gptkb:Certification
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
enclosed cockpit
|
|
gptkbp:controls
|
yoke control
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
low-wing monoplane
Chevron Aircraft Corporation team
|
|
gptkbp:engine
|
gptkb:musical
200 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
150 L
|
|
gptkbp:height
|
2.74 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Chevron B24
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
7.62 m
|
|
gptkbp:manufacturer
|
gptkb:Chevron_Aircraft_Corporation
|
|
gptkbp:marketed_as
|
gptkb:Chevron_B24
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
1,134 kg
|
|
gptkbp:notable_features
|
good fuel efficiency
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_history
|
used in private aviation
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:production_location
|
gptkb:United_States
|
|
gptkbp:production_years
|
gptkb:1971
gptkb:1975
|
|
gptkbp:propulsion
|
two-blade propeller
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:seating_capacity
|
2
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:speed
|
65 km/h
|
|
gptkbp:type
|
civil aircraft
|
|
gptkbp:wing_area
|
12.5 m²
|
|
gptkbp:wingspan
|
9.14 m
|