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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
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aluminum alloy
cargo and passenger transport
high-wing
regional aircraft
STOL (Short Takeoff and Landing) aircraft
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gptkbp:avionics
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modernized in later models
|
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gptkbp:capacity
|
up to 50 passengers
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|
gptkbp:crew
|
2
2 pilots
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gptkbp:decommissioned
|
various dates by operators
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gptkbp:design
|
De Havilland Canada design team
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gptkbp:engine
|
2
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gptkbp:engine_type
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gptkb:engine
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|
gptkbp:features
|
large cargo door
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gptkbp:first_flight
|
gptkb:1965
pressurized
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gptkbp:fuel_capacity
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5,000 liters
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gptkbp:historical_significance
|
used in various humanitarian missions
|
|
https://www.w3.org/2000/01/rdf-schema#label
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DHC-5 D
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gptkbp:is_used_by
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military and civilian operators
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gptkbp:landing_gear
|
tricycle gear
|
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gptkbp:length
|
24.8 meters
|
|
gptkbp:manufacturer
|
gptkb:De_Havilland_Canada
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gptkbp:material
|
aluminum alloy
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
500 meters
600 meters
22,680 kg
|
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gptkbp:notable_event
|
none widely reported
|
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gptkbp:number_built
|
approximately 100
|
|
gptkbp:operational_range
|
1,200 km with max payload
|
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gptkbp:primary_user
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gptkb:Canadian_Forces
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gptkbp:produced_by
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gptkb:battle
|
|
gptkbp:production_years
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1965-1988
|
|
gptkbp:propulsion
|
gptkb:4
constant speed propellers
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
up to 6,000 kg
|
|
gptkbp:service_ceiling
|
7,620 meters
|
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gptkbp:services
|
gptkb:1966
|
|
gptkbp:status
|
some still in service
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gptkbp:successor
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gptkb:DHC-6_Twin_Otter
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gptkbp:tail_type
|
T-tail
|
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gptkbp:variant
|
gptkb:DHC-5_Buffalo
|
|
gptkbp:wing_area
|
80.3 m²
|
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gptkbp:wingspan
|
28.9 meters
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gptkbp:bfsParent
|
gptkb:DHC-5_Buffalo
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gptkbp:bfsLayer
|
5
|