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gptkbp:instanceOf
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aircraft
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|
gptkbp:aircraft
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biplane
light aircraft
wooden structure
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gptkbp:capacity
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10 passengers
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gptkbp:cockpit
|
enclosed cockpit
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gptkbp:constructionMaterial
|
monocoque fuselage
|
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gptkbp:controls
|
elevators and ailerons
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gptkbp:crew
|
2
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gptkbp:design
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gptkb:Henri_Farman
1920s
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gptkbp:enginePower
|
450 hp
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|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1925
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gptkbp:fuelCapacity
|
500 liters
|
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gptkbp:headlights
|
conventional tail
|
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gptkbp:height
|
4.5 m
|
|
gptkbp:historicalSignificance
|
one of the first commercial airliners
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Farman F.1300
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gptkbp:influenced
|
later transport aircraft designs
|
|
gptkbp:influencedBy
|
Farman F.60 Goliath
|
|
gptkbp:landingGear
|
fixed landing gear
|
|
gptkbp:legacy
|
paved the way for modern airliners
various_airlines_in_Europe
|
|
gptkbp:length
|
20.5 m
|
|
gptkbp:manufacturer
|
gptkb:Farman_Aviation_Works
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
3000 kg
|
|
gptkbp:notableFeature
|
large cabin space
none widely reported.
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|
gptkbp:numberOfEpisodes
|
2
|
|
gptkbp:operationalHistory
|
used in commercial flights
|
|
gptkbp:primaryUser
|
civil aviation
|
|
gptkbp:productionYears
|
1925-1930
|
|
gptkbp:propulsion
|
two-blade propeller
|
|
gptkbp:range
|
800 km
|
|
gptkbp:retirementYear
|
1935
|
|
gptkbp:role
|
transport aircraft
|
|
gptkbp:services
|
1926
4000 m
|
|
gptkbp:successor
|
gptkb:Farman_F.2200
|
|
gptkbp:takeoffDistance
|
300 m
250 m
|
|
gptkbp:totalGoals
|
approximately 100
|
|
gptkbp:usedBy
|
gptkb:French_Air_Force
|
|
gptkbp:variant
|
gptkb:Farman_F.1301
|
|
gptkbp:weight
|
1800 kg
|
|
gptkbp:wingArea
|
80 m²
high-wing configuration
|
|
gptkbp:wingspan
|
28.5 m
|