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gptkbp:instance_of
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gptkb:aircraft
|
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gptkbp:aircraft_operated
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gptkb:aircraft
straight wing
72 kg/m²
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|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:climb_rate
|
3.5 m/s
|
|
gptkbp:cockpit
|
open cockpit
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gptkbp:controls
|
dual control
yoke control
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gptkbp:crew
|
1 pilot
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gptkbp:design
|
low-wing monoplane
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|
gptkbp:engine
|
Gipsy Major engine
|
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gptkbp:engine_type
|
piston engine
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gptkbp:financial_performance
|
high stability
|
|
gptkbp:first_flight
|
1946
|
|
gptkbp:flaps
|
split flaps
|
|
gptkbp:fuel_capacity
|
136 liters
|
|
gptkbp:height
|
2.54 m
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|
gptkbp:historical_significance
|
used in many air forces worldwide
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
DHC-1 A
|
|
gptkbp:instrumentation
|
basic flight instruments
|
|
gptkbp:introduced
|
1946
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|
gptkbp:is_used_by
|
gptkb:Royal_Canadian_Air_Force
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.23 m
|
|
gptkbp:manufacturer
|
gptkb:de_Havilland_Canada
|
|
gptkbp:material
|
gptkb:NACA_2412
metal construction
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:max_takeoff_weight
|
1,100 kg
1,200 kg
|
|
gptkbp:nickname
|
gptkb:mythological_figure
|
|
gptkbp:number_built
|
approximately 1,000
|
|
gptkbp:operational_history
|
used in various training programs.
|
|
gptkbp:origin
|
gptkb:Native_American_tribe
|
|
gptkbp:produced_by
|
1946-1956
|
|
gptkbp:propulsion
|
two-bladed propeller
0.12 k W/kg
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
2
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:speed
|
65 km/h
|
|
gptkbp:successor
|
gptkb:DHC-1_Chipmunk
|
|
gptkbp:surface
|
elevator, ailerons, rudder
|
|
gptkbp:tail_type
|
conventional tail
|
|
gptkbp:training
|
primary flight training
|
|
gptkbp:transportation
|
30 km/h
|
|
gptkbp:type
|
civilian trainer
|
|
gptkbp:variant
|
gptkb:DHC-1_B
|
|
gptkbp:wing_area
|
16.5 m²
|
|
gptkbp:wingspan
|
11.58 m
|
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gptkbp:bfsParent
|
gptkb:DHC-1_Chipmunk
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gptkbp:bfsLayer
|
6
|