|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:DHC-10-100
|
|
gptkbp:aircraft_operated
|
gptkb:DHC-10_family
15,000 kg
single aisle
regional aircraft
high-wing configuration
turboprop airliner
|
|
gptkbp:avionics
|
analog instruments
|
|
gptkbp:capacity
|
50 passengers
|
|
gptkbp:certification
|
gptkb:Transport_Canada
|
|
gptkbp:cockpit
|
two-pilot cockpit
|
|
gptkbp:crew
|
2 pilots
|
|
gptkbp:decommissioned
|
various years
|
|
gptkbp:design
|
high-wing monoplane
commuter aircraft
|
|
gptkbp:engine
|
1,000 hp
2 engines
|
|
gptkbp:engine_type
|
turboprop
Pratt & Whitney Canada P T6 A
|
|
gptkbp:first_flight
|
gptkb:1965
glass cockpit
|
|
gptkbp:fuel_capacity
|
5,000 liters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
DHC-10-100 A
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
25.6 meters
|
|
gptkbp:manufacturer
|
gptkb:De_Havilland_Canada
|
|
gptkbp:material
|
aluminum alloy
pressurized fuselage
|
|
gptkbp:max_speed
|
500 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 meters
1,500 meters
22,680 kg
|
|
gptkbp:notable_operations
|
gptkb:Air_Canada
|
|
gptkbp:number_built
|
over 100
|
|
gptkbp:production_years
|
1965-1980
|
|
gptkbp:propulsion
|
2
|
|
gptkbp:range
|
2,000 km
1,500 km
2,500 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
6,000 kg
regional routes
single-class or dual-class
|
|
gptkbp:service_ceiling
|
7,620 meters
|
|
gptkbp:services
|
gptkb:1966
|
|
gptkbp:speed
|
400 km/h
|
|
gptkbp:successor
|
gptkb:DHC-8
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:wing_area
|
70 m²
|
|
gptkbp:wingspan
|
28.4 meters
|