|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Mitsubishi_Type_13
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:item
twin-engine
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Mitsubishi_Aircraft_Company
high-wing monoplane
|
|
gptkbp:engine
|
2
300 hp
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
gptkb:1954
|
|
gptkbp:fuel_capacity
|
2,500 L
|
|
gptkbp:height
|
7.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi B28 M
|
|
gptkbp:introduced
|
gptkb:1954
|
|
gptkbp:is_used_by
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
22.8 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:material
|
gptkb:item
|
|
gptkbp:max_speed
|
350 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 m
800 m
8,000 kg
|
|
gptkbp:military_technology
|
gptkb:Company
charter flights
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:primary_user
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:production_location
|
gptkb:Japan
|
|
gptkbp:production_years
|
1954-1960
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
gptkb:28
|
|
gptkbp:service_ceiling
|
6,000 m
|
|
gptkbp:successor
|
gptkb:Mitsubishi_B-60
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
gptkb:Mitsubishi_B28_M-1
gptkb:Mitsubishi_B28_M-2
|
|
gptkbp:wing_area
|
70 m²
|
|
gptkbp:wingspan
|
28.0 m
|