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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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high-wing
twin-engine turboprop
light transport aircraft
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|
gptkbp:aspect_ratio
|
8.5
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gptkbp:avionics
|
modernized in 1980s
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gptkbp:capacity
|
up to 30 passengers
|
|
gptkbp:climb_rate
|
5 m/s
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|
gptkbp:cockpit
|
pressurized
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|
gptkbp:crew
|
2 pilots
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gptkbp:design
|
gptkb:Mitsubishi_Heavy_Industries
high-wing monoplane
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|
gptkbp:engine
|
2
1,000 hp per engine
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|
gptkbp:engine_type
|
turboprop
P T6 A-34
|
|
gptkbp:first_flight
|
gptkb:1970
two crew seats
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|
gptkbp:fuel_capacity
|
2,500 liters
|
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gptkbp:height
|
7.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi B600 M
|
|
gptkbp:interior_features
|
flexible seating arrangement
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
3.5 meters
22.8 meters
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
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|
gptkbp:market
|
regional aviation
|
|
gptkbp:material
|
aluminum alloy
22.8 meters
|
|
gptkbp:max_speed
|
450 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 meters
1,000 meters
8,000 kg
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_range
|
1,200 km with full load
|
|
gptkbp:primary_user
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:production_location
|
gptkb:Japan
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|
gptkbp:production_years
|
1970-1980
|
|
gptkbp:propulsion
|
gptkb:4
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirement_year
|
gptkb:1980s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
3,000 kg
large rear door
front entry door
|
|
gptkbp:service_ceiling
|
7,600 meters
|
|
gptkbp:services
|
gptkb:1971
|
|
gptkbp:speed
|
400 km/h
|
|
gptkbp:successor
|
gptkb:Mitsubishi_B800_M
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
B600 M-1
|
|
gptkbp:wing_area
|
70 m²
|
|
gptkbp:wingspan
|
28.5 meters
|