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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Cessna_210
|
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gptkbp:aircraft_operated
|
gptkb:aircraft
fixed-wing aircraft
single-engine land
N-number registered
|
|
gptkbp:avionics
|
modern avionics systems
|
|
gptkbp:category
|
general aviation
|
|
gptkbp:climb_rate
|
1,000 feet per minute
|
|
gptkbp:cockpit
|
pressurized cockpit
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
high-wing monoplane
|
|
gptkbp:discontinued
|
gptkb:1986
|
|
gptkbp:engine
|
gptkb:Continental_IO-520-U
300 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
102 gallons
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
gptkbp:height
|
2.74 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Cessna 210 N
|
|
gptkbp:introduced
|
gptkb:1970
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.53 m
|
|
gptkbp:manufacturer
|
gptkb:Cessna_Aircraft_Company
|
|
gptkbp:market_segment
|
private and business aviation
|
|
gptkbp:max_speed
|
160 knots
|
|
gptkbp:max_takeoff_weight
|
1,588 kg
|
|
gptkbp:notable_features
|
retractable landing gear
|
|
gptkbp:number_built
|
over 5,000
|
|
gptkbp:performance
|
high performance
|
|
gptkbp:production_years
|
1970-1986
|
|
gptkbp:propulsion
|
constant speed propeller
|
|
gptkbp:range
|
1,000 nautical miles
|
|
gptkbp:seating_capacity
|
gptkb:5
388 kg
|
|
gptkbp:service_ceiling
|
20,000 feet
|
|
gptkbp:speed
|
60 knots
150 knots
|
|
gptkbp:successor
|
gptkb:Cessna_210_R
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:type
|
single-engine aircraft
|
|
gptkbp:variant
|
gptkb:Cessna_210
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:wing_area
|
16.2 m²
|
|
gptkbp:wingspan
|
11.13 m
|