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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Canadian_Air_Force
|
|
gptkbp:aircraft_operated
|
gptkb:DHC-6_family
aluminum
twin-engine
regional aircraft
|
|
gptkbp:crew
|
2
|
|
gptkbp:current_use
|
various airlines and military forces
|
|
gptkbp:design
|
high-wing monoplane
DHC engineering team
|
|
gptkbp:engine
|
2
680 hp
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:first_flight
|
gptkb:1965
|
|
gptkbp:fuel_capacity
|
1,200 L
|
|
gptkbp:height
|
4.93 m
|
|
gptkbp:historical_significance
|
pioneered STOL capabilities
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CC-138 Twin Otter
|
|
gptkbp:influences
|
STOL aircraft design
|
|
gptkbp:is_used_by
|
gptkb:Canadian_Forces
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
14.73 m
|
|
gptkbp:manufacturer
|
gptkb:De_Havilland_Canada
|
|
gptkbp:market_segment
|
regional aviation
|
|
gptkbp:material
|
aluminum
|
|
gptkbp:max_speed
|
200 knots
|
|
gptkbp:max_takeoff_weight
|
1,200 ft
1,000 ft
5,670 kg
|
|
gptkbp:modifications
|
floatplane version available
|
|
gptkbp:nickname
|
gptkb:Twin_Otter
|
|
gptkbp:notable_event
|
none widely reported
|
|
gptkbp:notable_features
|
short takeoff and landing capabilities
|
|
gptkbp:operational_area
|
passenger and cargo transport
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:operator
|
gptkb:Province
|
|
gptkbp:primary_user
|
airlines, military, charter operators
|
|
gptkbp:produced_by
|
over 900 units
|
|
gptkbp:production_years
|
1965-1988
|
|
gptkbp:propulsion
|
variable-pitch propellers
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retirement_year
|
still in service
|
|
gptkbp:role
|
utility transport
|
|
gptkbp:safety_record
|
generally good
|
|
gptkbp:seating_capacity
|
gptkb:19
1,500 kg
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:services
|
gptkb:1966
|
|
gptkbp:speed
|
180 knots
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:type
|
STOL aircraft
|
|
gptkbp:variant
|
gptkb:DHC-6-300
|
|
gptkbp:wing_area
|
30.5 m²
|
|
gptkbp:wingspan
|
19.81 m
|