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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Mitsubishi_Type_13
|
|
gptkbp:aircraft_operated
|
fixed-wing aircraft
high-wing
|
|
gptkbp:cockpit
|
tandem cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:public_transportation_system
production
|
|
gptkbp:engine
|
2
300 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:first_released
|
gptkb:1956
1970s
|
|
gptkbp:fuel_capacity
|
1,500 L
|
|
gptkbp:height
|
8.0 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi B91 M
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
22.5 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
5,500 kg
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_history
|
gptkb:Japan
|
|
gptkbp:origin
|
gptkb:Japan
|
|
gptkbp:primary_user
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirement_year
|
1970s
|
|
gptkbp:role
|
gptkb:aircraft
passenger transport
cargo transport
medical evacuation
|
|
gptkbp:seating_capacity
|
gptkb:television_series
1,500 kg
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:services
|
gptkb:1956
|
|
gptkbp:speed
|
80 km/h
|
|
gptkbp:successor
|
gptkb:Mitsubishi_YS-11
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
B91 M-1
B91 M-2
|
|
gptkbp:wingspan
|
30.0 m
|