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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:aspect_ratio
|
6.5
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|
gptkbp:cargo_capacity
|
1,500 kg
|
|
gptkbp:climb_rate
|
1,200 ft/min
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|
gptkbp:control_surfaces
|
elevator, ailerons, rudder
|
|
gptkbp:crew
|
1-2
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|
gptkbp:design
|
De Havilland Canada design team
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|
gptkbp:engine
|
gptkb:Pratt_&_Whitney_Canada_PT6_A
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|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:financial_stability
|
good low-speed stability
|
|
gptkbp:first_flight
|
1965-05-20
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|
gptkbp:flaps
|
full-span flaps
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|
gptkbp:fuel_capacity
|
1,200 L
|
|
gptkbp:height
|
6.93 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
De Havilland Canada DHC-6 Twin Otter
|
|
gptkbp:introduced
|
gptkb:1965
|
|
gptkbp:is_popular_for
|
bush flying
|
|
gptkbp:landing_distance
|
1,000 ft
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
15.85 m
|
|
gptkbp:manufacturer
|
gptkb:De_Havilland_Canada
|
|
gptkbp:max_speed
|
180 knots
|
|
gptkbp:max_takeoff_weight
|
5,670 kg
|
|
gptkbp:notable_features
|
versatile and rugged design
|
|
gptkbp:notable_operators
|
gptkb:Bristow_Group
gptkb:Air_Canada
gptkb:Alaska_Airlines
gptkb:Canadian_Forces
gptkb:Sky_West_Airlines
|
|
gptkbp:number_built
|
over 1,000
|
|
gptkbp:operational_history
|
used in various roles worldwide.
|
|
gptkbp:passenger_capacity
|
gptkb:19
|
|
gptkbp:primary_function
|
short takeoff and landing
|
|
gptkbp:production_years
|
gptkb:1988
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retired
|
still in service in some operators
|
|
gptkbp:role
|
STOL aircraft
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:service_entry
|
gptkb:1966
|
|
gptkbp:successor
|
gptkb:DHC-6_Series_400
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:takeoff_distance
|
1,200 ft
|
|
gptkbp:used_in
|
gptkb:civil_aviation
gptkb:military_aircraft
|
|
gptkbp:variant
|
gptkb:DHC-6-100
gptkb:DHC-6-200
gptkb:DHC-6-300
gptkb:DHC-6-400
|
|
gptkbp:wing_area
|
30.5 m²
|
|
gptkbp:wing_configuration
|
high-wing
|
|
gptkbp:wingspan
|
19.81 m
|
|
gptkbp:bfsParent
|
gptkb:C-12_Huron
|
|
gptkbp:bfsLayer
|
4
|