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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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7
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gptkbp:bfsParent
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gptkb:Mitsubishi_B85_M
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gptkbp:aircraft_operated
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gptkb:starship
commercial aviation
fixed-wing aircraft
advanced avionics
lightweight design
high reliability
utility aircraft
single-deck
high-wing
detailed technical specifications
developed for regional airlines
B400 M-1, B400 M-2
part of Mitsubishi's aviation legacy
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gptkbp:avionics
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modern navigation systems
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gptkbp:capacity
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up to 4000 kg
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gptkbp:combat_role
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gptkb:aircraft
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gptkbp:crew
|
2
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gptkbp:date
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gptkb:1975
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gptkbp:design
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gptkb:Mitsubishi_Heavy_Industries
cargo transport
high-wing monoplane
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gptkbp:engine
|
2
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gptkbp:engine_type
|
turboprop
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gptkbp:environmental_impact
|
low emissions
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gptkbp:first_flight
|
gptkb:1980
two-pilot cockpit
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gptkbp:fuel_capacity
|
3000 L
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|
https://www.w3.org/2000/01/rdf-schema#label
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Mitsubishi B400 M
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gptkbp:landing_gear
|
tricycle type
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gptkbp:length
|
24.0 m
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gptkbp:maintenance
|
relatively easy
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gptkbp:manufacturer
|
gptkb:Mitsubishi
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gptkbp:market
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gptkb:Asia
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|
gptkbp:material
|
aluminum alloy
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gptkbp:max_speed
|
500 km/h
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gptkbp:max_takeoff_weight
|
short takeoff and landing
12000 kg
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|
gptkbp:notable_users
|
gptkb:Japan_Air_Self-Defense_Force
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|
gptkbp:operational_history
|
used in various missions
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|
gptkbp:operational_range
|
regional operations
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|
gptkbp:production_location
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gptkb:Japan
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|
gptkbp:production_years
|
1980-1990
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|
gptkbp:propulsion
|
4-blade
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|
gptkbp:range
|
2000 km
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|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:safety_record
|
generally safe
|
|
gptkbp:seating_capacity
|
large volume
large rear cargo door
up to 30 passengers
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|
gptkbp:service_ceiling
|
8000 m
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gptkbp:successor
|
gptkb:Mitsubishi_B500_M
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|
gptkbp:tail_type
|
T-tail
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gptkbp:type
|
regional aircraft
|
|
gptkbp:weight
|
7000 kg
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|
gptkbp:wing_area
|
100 m²
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|
gptkbp:wingspan
|
30.0 m
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