|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Canadian_Air_Force
|
|
gptkbp:aircraft_operated
|
gptkb:DHC-1_Chipmunk
gptkb:DHC-3_Otter
gptkb:DHC-4_Caribou
|
|
gptkbp:avionics
|
modern avionics suite
|
|
gptkbp:certification
|
Type Certificate issued by Transport Canada
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:cockpit
|
pressurized cockpit
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
high-wing monoplane
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:first_flight
|
gptkb:1956
|
|
gptkbp:fuel_capacity
|
1,500 L
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
DHC-22 Dash 22
|
|
gptkbp:introduced
|
gptkb:1956
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
12.80 m
|
|
gptkbp:manufacturer
|
gptkb:De_Havilland_Canada
|
|
gptkbp:market
|
civil and military markets
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
3,600 kg
|
|
gptkbp:number_built
|
approximately 100
|
|
gptkbp:operational_area
|
low operational cost
|
|
gptkbp:operational_history
|
used in various roles including transport and reconnaissance.
|
|
gptkbp:power_output
|
Pratt & Whitney Canada P T6 A
|
|
gptkbp:primary_user
|
gptkb:Canadian_military
|
|
gptkbp:production_years
|
1956-1960
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
gptkb:1980s
|
|
gptkbp:role
|
utility aircraft
|
|
gptkbp:safety_record
|
good safety record
|
|
gptkbp:seating_capacity
|
gptkb:6
1,000 kg
|
|
gptkbp:service_ceiling
|
7,620 m
|
|
gptkbp:successor
|
gptkb:DHC-6_Twin_Otter
|
|
gptkbp:variant
|
gptkb:DHC-22_A
gptkb:DHC-22_B
|
|
gptkbp:weight
|
2,200 kg
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
15.85 m
|