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gptkbp:instanceOf
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aircraft
|
|
gptkbp:aircraft
|
high-wing
|
|
gptkbp:armament
|
none
|
|
gptkbp:avionics
|
analog avionics
|
|
gptkbp:capacity
|
10 passengers
|
|
gptkbp:cockpit
|
pressurized cockpit
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Mitsubishi_Aircraft_Corporation
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:fuelCapacity
|
1,200 liters
|
|
gptkbp:height
|
4.1 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mitsubishi M-28
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi
|
|
gptkbp:maxSpeed
|
300 km/h
|
|
gptkbp:maxTakeoffWeight
|
3,500 kg
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:numberOfEpisodes
|
2
|
|
gptkbp:operationalHistory
|
used in various roles
|
|
gptkbp:primaryUser
|
gptkb:Japan_Air_Self-Defense_Force
|
|
gptkbp:productionYears
|
1955-1960
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirementYear
|
1970
|
|
gptkbp:role
|
transport aircraft
cargo_aircraft
|
|
gptkbp:services
|
6,000 m
|
|
gptkbp:successor
|
gptkb:Mitsubishi_M-30
|
|
gptkbp:variant
|
gptkb:M-28B
M-28A
|
|
gptkbp:wingspan
|
15.5 m
|