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gptkbp:instanceOf
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aircraft
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gptkbp:aircraft
|
retired
civil aviation
monoplane
utility aircraft
conventional tail
pioneering design in aviation history
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gptkbp:cockpit
|
open cockpit
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gptkbp:constructionMaterial
|
metal construction
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gptkbp:controls
|
ailerons
elevator
rudder
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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
|
300 hp
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gptkbp:engineType
|
piston engine
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gptkbp:firstFlight
|
1925
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gptkbp:firstGeneration
|
1926
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gptkbp:fuelCapacity
|
600 L
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gptkbp:headlights
|
conventional tail
|
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gptkbp:height
|
4.0 m
|
|
gptkbp:historicalSignificance
|
early commercial aviation
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|
https://www.w3.org/2000/01/rdf-schema#label
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Farman F.800
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gptkbp:influencedBy
|
gptkb:Farman_F.60
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gptkbp:landingGear
|
tailwheel
|
|
gptkbp:length
|
14.0 m
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gptkbp:manufacturer
|
gptkb:Farman_Aviation_Works
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
3,000 kg
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gptkbp:notableFeature
|
high-wing monoplane
crash in 1928
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|
gptkbp:numberOfEpisodes
|
2
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gptkbp:passengerCapacity
|
8
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gptkbp:primaryUser
|
gptkb:French_Air_Force
|
|
gptkbp:productionCompany
|
50
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gptkbp:productionLocation
|
gptkb:France
|
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gptkbp:productionYears
|
1925-1930
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|
gptkbp:range
|
1,000 km
|
|
gptkbp:retirementYear
|
1930
|
|
gptkbp:role
|
transport aircraft
|
|
gptkbp:services
|
4,500 m
|
|
gptkbp:successor
|
gptkb:Farman_F.100
|
|
gptkbp:usedIn
|
aerial photography
passenger transport
cargo transport
military reconnaissance
|
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gptkbp:variant
|
gptkb:Farman_F.801
|
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gptkbp:weight
|
1,800 kg
|
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gptkbp:wingArea
|
70 m²
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gptkbp:wingspan
|
20.0 m
|