|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Mitsubishi_Type_13
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
fixed-wing aircraft
high-wing
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:capacity
|
20 passengers
|
|
gptkbp:cockpit
|
pressurized cockpit
|
|
gptkbp:combat_role
|
transport and logistics
|
|
gptkbp:crew
|
2
2 pilots
|
|
gptkbp:design
|
gptkb:Mitsubishi_Aircraft_Company
Mitsubishi engineers
|
|
gptkbp:engine
|
2
600 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
1950
|
|
gptkbp:fuel_capacity
|
2000 L
|
|
gptkbp:height
|
8.0 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi B71 M
|
|
gptkbp:is_used_by
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
22.5 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
600 m
800 m
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_history
|
served in the 1950s and 1960s.
|
|
gptkbp:operational_range
|
1500 km
|
|
gptkbp:primary_user
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:production_years
|
1950-1955
|
|
gptkbp:propulsion
|
twin-engine
variable-pitch propeller
|
|
gptkbp:range
|
2000 km
|
|
gptkbp:retirement_year
|
1960s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
2000 kg
single-class seating
|
|
gptkbp:service_ceiling
|
8000 m
|
|
gptkbp:services
|
1951
|
|
gptkbp:successor
|
gptkb:Mitsubishi_YS-11
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
gptkb:Mitsubishi_B71_M-1
|
|
gptkbp:weight
|
5000 kg
|
|
gptkbp:wing_area
|
100 m²
|
|
gptkbp:wingspan
|
30.0 m
|