|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
twin-engine
|
|
gptkbp:aircraft_operated
|
gptkb:transport_aircraft
retired
20,000 kg
400 km/h
8.0 m
24.5 m
|
|
gptkbp:aircraft_role
|
utility aircraft
|
|
gptkbp:aircraft_type
|
fixed-wing aircraft
|
|
gptkbp:built
|
50
|
|
gptkbp:capacity
|
up to 30 passengers
|
|
gptkbp:cockpit
|
pressurized cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Mitsubishi_Aircraft_Corporation
|
|
gptkbp:engine
|
2
|
|
gptkbp:engine_power
|
1,200 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:fuselage_material
|
gptkb:metal
|
|
gptkbp:height
|
8.0 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi B63 M-1
|
|
gptkbp:introduced
|
gptkb:1955
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
24.5 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
20,000 kg
|
|
gptkbp:military_service
|
gptkb:Japan
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:passenger_capacity
|
gptkb:30
|
|
gptkbp:primary_user
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:produces
|
limited production
|
|
gptkbp:production_years
|
1955-1960
|
|
gptkbp:propeller
|
variable-pitch propellers
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:related_aircraft
|
gptkb:Mitsubishi_Ki-67_Hiryu
Mitsubishi B-26 Marauder
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
gptkb:transport_aircraft
gptkb:aircraft
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:successor
|
gptkb:Mitsubishi_B-70
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
B63 M-1 A
B63 M-1 B
|
|
gptkbp:wing_configuration
|
gptkb:metal
high-wing configuration
|
|
gptkbp:wingspan
|
30.0 m
|
|
gptkbp:bfsParent
|
gptkb:Mitsubishi_B63_M
|
|
gptkbp:bfsLayer
|
7
|