gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:aircraft_configuration
|
gptkb:monoplane
|
gptkbp:aircraft_operated
|
4 hours
fixed-wing aircraft
2,500 lbs
|
gptkbp:aircraft_type
|
civil aircraft
|
gptkbp:avionics
|
varies by installation
|
gptkbp:category
|
general aviation
|
gptkbp:climb_rate
|
1,000 ft/min
|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
gptkbp:control_system
|
yoke and rudder pedals
|
gptkbp:crew
|
1 pilot
|
gptkbp:cruise_speed
|
140 knots
|
gptkbp:design
|
personal and business travel
|
gptkbp:design_features
|
tapered wings
|
gptkbp:engine_configuration
|
horizontally opposed
|
gptkbp:engine_power
|
260 hp
|
gptkbp:engine_type
|
gptkb:Continental_IO-520
piston engine
|
gptkbp:first_flight
|
gptkb:1960
|
gptkbp:fuel_capacity
|
65 gallons
|
gptkbp:fuel_type
|
aviation gasoline
|
gptkbp:height
|
8 ft 10 in
|
gptkbp:historical_significance
|
popular among private pilots.
|
https://www.w3.org/2000/01/rdf-schema#label
|
Cessna 210 C
|
gptkbp:is_often_used_in
|
flight training
|
gptkbp:landing_distance
|
65 knots
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
27 ft 2 in
|
gptkbp:manufacturer
|
gptkb:Cessna_Aircraft_Company
|
gptkbp:market_segment
|
gptkb:light_aircraft
|
gptkbp:max_speed
|
160 knots
|
gptkbp:max_takeoff_weight
|
3,600 lbs
|
gptkbp:notable_features
|
high-wing design
|
gptkbp:number_built
|
over 5,000 units
|
gptkbp:orbital_altitude
|
10,000 ft
8,000 ft
|
gptkbp:passenger_capacity
|
5 passengers
|
gptkbp:power_consumption
|
13.8 lbs/hp
|
gptkbp:price
|
approximately $20,000
|
gptkbp:production_years
|
1960-1970
|
gptkbp:propeller
|
constant-speed propeller
|
gptkbp:range
|
1,000 miles
1,000 nautical miles
|
gptkbp:service_ceiling
|
20,000 ft
|
gptkbp:stall_speed
|
60 knots
|
gptkbp:successor
|
gptkb:Cessna_210_N
|
gptkbp:takeoff_distance
|
1,500 ft
|
gptkbp:type
|
single-engine aircraft
|
gptkbp:wing_area
|
174 sq ft
|
gptkbp:wing_configuration
|
20.7 lbs/sq ft
|
gptkbp:wingspan
|
36 ft 0 in
|
gptkbp:bfsParent
|
gptkb:Continental_IO-360
|
gptkbp:bfsLayer
|
8
|