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gptkbp:instanceOf
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aircraft
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gptkbp:aircraft
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single-engine aircraft
conventional tail
high-wing
light sport aircraft
cantilever wing
stable and forgiving
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gptkbp:avionics
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basic avionics package
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gptkbp:built
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over 1,000
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gptkbp:cockpit
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two-seat cockpit
side-by-side seating
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gptkbp:constructionMaterial
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metal and composite
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gptkbp:covers
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manual flaps
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gptkbp:crew
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1
used for flight training
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gptkbp:design
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gptkb:Jean-Pierre_Robin
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gptkbp:engine
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piston engine
front-mounted engine
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gptkbp:engineType
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Lycoming O-360
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gptkbp:firstFlight
|
1972
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gptkbp:fuel_capacity
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100 L
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gptkbp:headlights
|
T-tail
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gptkbp:height
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2.1 m
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https://www.w3.org/2000/01/rdf-schema#label
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Robin DR400
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gptkbp:IATA_code
|
enthusiast community
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gptkbp:instrument
|
analog instruments
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gptkbp:is_popular_among
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Europe
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gptkbp:landing_gear
|
tricycle gear
fixed landing gear
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gptkbp:length
|
7.2 m
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gptkbp:manufacturer
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gptkb:Robin_Aircraft
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gptkbp:market_segment
|
private pilots
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gptkbp:maximum_speed
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220 km/h
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gptkbp:maxTakeoffWeight
|
1,200 kg
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gptkbp:notableUsers
|
flying schools
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gptkbp:origin
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gptkb:France
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gptkbp:passengerCapacity
|
3
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gptkbp:performances
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relatively low maintenance costs
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gptkbp:productionYears
|
1972-present
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gptkbp:propulsion
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variable-pitch propeller
2 blades
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gptkbp:range
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1,000 km
|
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gptkbp:role
|
general aviation
|
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gptkbp:service_ceiling
|
5,000 m
|
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gptkbp:speed
|
200 km/h
60 km/h
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gptkbp:surface
|
elevator
rudder
aileron
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gptkbp:surrounding_area
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12.5 m²
|
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gptkbp:takeoffDistance
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300 m
400 m
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gptkbp:type
|
light aircraft
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gptkbp:variant
|
DR400/120,_DR400/180,_DR400/200
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gptkbp:weight
|
750 kg
450 kg
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gptkbp:wingspan
|
9.1 m
|