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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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6
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gptkbp:bfsParent
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gptkb:Mitsubishi_Type_13
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gptkbp:aircraft_operated
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gptkb:aircraft
transport and logistics
high-wing
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|
gptkbp:armament
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gptkb:none
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gptkbp:avionics
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modernized for military use
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gptkbp:capacity
|
up to 30 passengers
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|
gptkbp:combat_role
|
logistics support
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gptkbp:crew
|
2
2 pilots
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|
gptkbp:design
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gptkb:Mitsubishi_Heavy_Industries
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|
gptkbp:emergency_services
|
multiple exits
|
|
gptkbp:engine
|
2
1,800 hp per engine
|
|
gptkbp:engine_type
|
turboprop
P W100 series
|
|
gptkbp:features
|
short takeoff and landing capabilities
|
|
gptkbp:first_flight
|
gptkb:1981
gptkb:2000
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|
gptkbp:fuel_capacity
|
5,000 liters
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi B81 M
|
|
gptkbp:interior_features
|
2.0 meters
|
|
gptkbp:landing_gear
|
tricycle type
|
|
gptkbp:length
|
24.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:material
|
aluminum alloy
|
|
gptkbp:max_speed
|
500 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 meters
1,000 meters
20,000 kg
|
|
gptkbp:modifications
|
upgraded avionics
|
|
gptkbp:notable_features
|
large cargo door
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_history
|
served in various missions
|
|
gptkbp:operational_range
|
1,500 km with full load
|
|
gptkbp:primary_user
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:production_years
|
1981-1990
|
|
gptkbp:propulsion
|
variable pitch
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:retirement_year
|
gptkb:2000
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
3,000 kg
30 seats
flexible interior layout
2.5 x 2.0 meters
|
|
gptkbp:service_ceiling
|
7,600 meters
|
|
gptkbp:services
|
gptkb:1983
20 years
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Mitsubishi_B90_M
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
B81 M-1
|
|
gptkbp:width
|
2.5 meters
|
|
gptkbp:wing_area
|
70 m²
|
|
gptkbp:wingspan
|
28.0 meters
|