|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Dash_8_family
|
|
gptkbp:aircraft_operated
|
DHC-7 family
|
|
gptkbp:certification
|
TC 7 A-1
|
|
gptkbp:climb_rate
|
5.5 m/s
|
|
gptkbp:crew
|
2
|
|
gptkbp:customer_support
|
gptkb:Air_Canada
|
|
gptkbp:design
|
high-wing
De Havilland Canada design team
|
|
gptkbp:engine
|
Pratt & Whitney Canada P T6 A-50
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:first_flight
|
2020-12-31
1975-03-27
|
|
gptkbp:fuel_capacity
|
5,000 L
|
|
gptkbp:height
|
8.38 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
De Havilland Canada DHC-7
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
25.77 m
|
|
gptkbp:manufacturer
|
gptkb:De_Havilland_Canada
|
|
gptkbp:max_speed
|
550 km/h
|
|
gptkbp:max_takeoff_weight
|
900 m
1,200 m
22,680 kg
|
|
gptkbp:notable_operations
|
gptkb:aircraft
gptkb:Air_Canada
gptkb:Royal_Canadian_Air_Force
gptkb:Alaska_Airlines
gptkb:Canadian_Forces
|
|
gptkbp:number_built
|
gptkb:113
|
|
gptkbp:production_years
|
1975-1988
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
gptkb:2005
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
50
3,000 kg
4,500 kg
|
|
gptkbp:service_ceiling
|
7,620 m
|
|
gptkbp:services
|
1978-01-01
|
|
gptkbp:speed
|
100 km/h
|
|
gptkbp:successor
|
gptkb:De_Havilland_Canada_DHC-8
|
|
gptkbp:variant
|
gptkb:DHC-7-100
gptkb:DHC-7-200
DHC-7-300
DHC-7-102
DHC-7-103
|
|
gptkbp:wing_area
|
75.5 m²
|
|
gptkbp:wingspan
|
28.96 m
|
|
gptkbp:year_created
|
gptkb:1978
|