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gptkbp:instanceOf
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aircraft
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gptkbp:aircraft
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retired
light aircraft
cantilever wing
multi-purpose aircraft
single fuselage
commuter_aircraft
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gptkbp:cockpit
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enclosed cockpit
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gptkbp:controls
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elevator, ailerons, rudder
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gptkbp:countryOfOrigin
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gptkb:France
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gptkbp:crewCapacity
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2
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gptkbp:design
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gptkb:Henri_Farman
1940s
low drag design
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gptkbp:enginePower
|
300 hp
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gptkbp:engineType
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piston engine
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gptkbp:firstFlight
|
1946
1946-07-01
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gptkbp:fuelCapacity
|
800 L
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gptkbp:height
|
4.0 m
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|
gptkbp:helicopterCapacity
|
two-seat cockpit
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gptkbp:historicalSignificance
|
one of the first post-war aircraft
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|
https://www.w3.org/2000/01/rdf-schema#label
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Farman F.2401
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gptkbp:influences
|
inspired later designs
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gptkbp:landingGear
|
tricycle gear
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gptkbp:legacy
|
contributed to aviation development
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gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Farman_Aviation_Works
|
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gptkbp:maxSpeed
|
250 km/h
|
|
gptkbp:maxTakeoffWeight
|
3,000 kg
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gptkbp:notableFeature
|
spacious cabin
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gptkbp:notableUsers
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gptkb:French_Air_Force
|
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gptkbp:numberBuilt
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20
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gptkbp:numberOfEpisodes
|
2
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gptkbp:operationalHistory
|
used in regional flights
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gptkbp:passengerCapacity
|
6
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gptkbp:productionLocation
|
gptkb:France
|
|
gptkbp:productionYears
|
1946-1950
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gptkbp:propulsion
|
variable-pitch propeller
|
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gptkbp:range
|
1,000 km
|
|
gptkbp:retirementYear
|
1950
|
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gptkbp:role
|
civil aviation
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:setting
|
high-wing monoplane
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gptkbp:speed
|
200 km/h
|
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gptkbp:takeoffDistance
|
300 m
400 m
|
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gptkbp:type
|
transport aircraft
|
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gptkbp:weight
|
1,500 kg
|
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gptkbp:wingArea
|
30 m²
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gptkbp:wingspan
|
15.5 m
|