|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Mitsubishi_Type_13
|
|
gptkbp:aircraft_operated
|
gptkb:public_transportation_system
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:cockpit
|
pressurized
|
|
gptkbp:combat_role
|
gptkb:Company
|
|
gptkbp:constructed_in
|
50
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:crew
|
2
|
|
gptkbp:decommissioned
|
gptkb:1995
|
|
gptkbp:design
|
gptkb:Mitsubishi_Heavy_Industries
Mitsubishi engineers
|
|
gptkbp:developer
|
1955-1959
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_type
|
gptkb:Rolls-Royce_Dart
turboprop
|
|
gptkbp:features
|
high-wing configuration
|
|
gptkbp:first_flight
|
gptkb:1959
gptkb:2000
|
|
gptkbp:first_released
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
8,000 liters
|
|
gptkbp:height
|
8.0 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi B59 M
|
|
gptkbp:influenced_by
|
gptkb:Douglas_DC-3
|
|
gptkbp:is_used_by
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
25.5 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:material
|
metallic alloys
|
|
gptkbp:max_speed
|
500 km/h
|
|
gptkbp:max_takeoff_weight
|
30,000 kg
|
|
gptkbp:notable_features
|
large cargo door
|
|
gptkbp:operational_history
|
served in various roles
|
|
gptkbp:operational_range
|
1,500 km with max payload
|
|
gptkbp:primary_user
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:propulsion
|
variable-pitch
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:retirement_year
|
replacement by modern aircraft
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:safety_record
|
generally safe
|
|
gptkbp:seating_capacity
|
up to 30
5,000 kg
|
|
gptkbp:service_ceiling
|
7,500 m
|
|
gptkbp:successor
|
gptkb:Mitsubishi_YS-11
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:used_in
|
disaster relief missions
|
|
gptkbp:variant
|
B59 M-1
|
|
gptkbp:wing_area
|
100 m²
|
|
gptkbp:wingspan
|
30.0 m
|