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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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5
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gptkbp:bfsParent
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gptkb:DHC-25_Dash_25
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:DHC-2_family
utility aircraft
high-wing
varied by operator
retired from active service
influenced future utility aircraft designs
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gptkbp:cockpit
|
enclosed cockpit
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gptkbp:crew
|
2
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gptkbp:design
|
high-wing monoplane
De Havilland engineers
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gptkbp:engine
|
gptkb:Lycoming_O-540
|
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gptkbp:engine_type
|
piston engine
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|
gptkbp:financial_performance
|
good stability and control
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gptkbp:first_flight
|
gptkb:1952
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|
gptkbp:flaps
|
split flaps
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|
gptkbp:fuel_capacity
|
300 L
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gptkbp:height
|
3.05 m
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|
gptkbp:historical_significance
|
used in various roles during its service life
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|
https://www.w3.org/2000/01/rdf-schema#label
|
DHC-25 C
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|
gptkbp:influenced_by
|
DHC-2 Beaver design principles
|
|
gptkbp:is_used_by
|
gptkb:military_unit
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
10.67 m
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|
gptkbp:manufacturer
|
gptkb:De_Havilland_Canada
|
|
gptkbp:market
|
civil and military markets
|
|
gptkbp:max_speed
|
250 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
250 m
3,175 kg
|
|
gptkbp:notable_features
|
short takeoff and landing capabilities
|
|
gptkbp:number_built
|
approximately 200
|
|
gptkbp:operational_history
|
served in various countries
|
|
gptkbp:operational_range
|
1,200 km
|
|
gptkbp:primary_user
|
gptkb:Canadian_military
|
|
gptkbp:production_location
|
gptkb:Native_American_tribe
|
|
gptkbp:production_years
|
1952-1956
|
|
gptkbp:propulsion
|
constant-speed propeller
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retirement_year
|
1970s
|
|
gptkbp:role
|
gptkb:aircraft
utility aircraft
|
|
gptkbp:seating_capacity
|
gptkb:6
1,200 kg
large rear cargo door
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:successor
|
gptkb:DHC-6_Twin_Otter
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
gptkb:DHC-2_Beaver
|
|
gptkbp:wing_area
|
30.0 m²
|
|
gptkbp:wingspan
|
12.80 m
|