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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:DHC-22_Dash_22
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gptkbp:aircraft_operated
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gptkb:aircraft
fixed-wing aircraft
lightweight design
single-engine configuration
influenced future aircraft designs.
good short takeoff and landing performance
part of the DHC family of aircraft
utility aircraft category
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|
gptkbp:cockpit
|
enclosed cockpit
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|
gptkbp:crew
|
2
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gptkbp:design
|
versatile utility operations
Walter J. Mc Curdy
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|
gptkbp:engine
|
gptkb:Lycoming_O-360_engine
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:features
|
rugged construction
|
|
gptkbp:financial_performance
|
good stability and control
|
|
gptkbp:first_flight
|
1946
|
|
gptkbp:flaps
|
split flaps
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|
gptkbp:fuel_capacity
|
200 liters
|
|
gptkbp:historical_significance
|
used in various roles including bush flying
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
DHC-22 A
|
|
gptkbp:influenced_by
|
DHC-2 Beaver design
|
|
gptkbp:is_used_by
|
gptkb:aircraft
|
|
gptkbp:landing_gear
|
tailwheel
|
|
gptkbp:length
|
9.1 m
|
|
gptkbp:manufacturer
|
gptkb:De_Havilland_Canada
|
|
gptkbp:market
|
general aviation market
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
1,500 kg
|
|
gptkbp:notable_features
|
high-wing monoplane
|
|
gptkbp:notable_users
|
gptkb:Province
|
|
gptkbp:number_built
|
approximately 100
|
|
gptkbp:operational_area
|
used for cargo and passenger transport
|
|
gptkbp:operational_history
|
served in various countries
|
|
gptkbp:origin
|
gptkb:Native_American_tribe
|
|
gptkbp:production_location
|
gptkb:Native_American_tribe
|
|
gptkbp:production_years
|
1946-1950
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retirement_year
|
retired from service in the 1970s
|
|
gptkbp:role
|
utility aircraft
|
|
gptkbp:seating_capacity
|
gptkb:6
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:successor
|
gptkb:DHC-3_Otter
|
|
gptkbp:surface
|
elevator and ailerons
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:variant
|
gptkb:DHC-2_Beaver
|
|
gptkbp:weight
|
900 kg
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
12.8 m
|