|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:DHC-27_Dash_27
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:DHC-3_Otter
twin-engine
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:certification
|
TC-1
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:combat_role
|
gptkb:public_transportation_system
|
|
gptkbp:crew
|
2
required
|
|
gptkbp:design
|
multi-role
|
|
gptkbp:engine
|
2
1,200 hp
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:features
|
high-wing configuration
|
|
gptkbp:first_flight
|
gptkb:1965
|
|
gptkbp:fuel_capacity
|
1,500 L
|
|
gptkbp:historical_significance
|
gptkb:aircraft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
DHC-27 A
|
|
gptkbp:influenced_by
|
gptkb:DHC-6_Twin_Otter
|
|
gptkbp:is_used_by
|
gptkb:military_unit
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
15.24 m
|
|
gptkbp:manufacturer
|
gptkb:De_Havilland_Canada
|
|
gptkbp:max_speed
|
370 km/h
|
|
gptkbp:max_takeoff_weight
|
900 m
1,200 m
5,400 kg
|
|
gptkbp:notable_features
|
short takeoff and landing capabilities
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_history
|
used in various missions
|
|
gptkbp:operational_range
|
1,200 km
|
|
gptkbp:origin
|
gptkb:Native_American_tribe
|
|
gptkbp:primary_user
|
gptkb:military_officer
|
|
gptkbp:production_years
|
1965-1970
|
|
gptkbp:propulsion
|
variable-pitch
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirement_year
|
gptkb:1970
|
|
gptkbp:role
|
utility aircraft
|
|
gptkbp:seating_capacity
|
gptkb:10
1,500 kg
|
|
gptkbp:service_ceiling
|
7,620 m
|
|
gptkbp:services
|
gptkb:1966
|
|
gptkbp:successor
|
gptkb:DHC-8
|
|
gptkbp:supports
|
certified
|
|
gptkbp:variant
|
gptkb:DHC-6_Twin_Otter
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
19.81 m
|