|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
high-wing monoplane
civil aircraft
cantilever wing
|
|
gptkbp:armament
|
none
|
|
gptkbp:cabinType
|
passenger cabin
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:constructionMaterial
|
monocoque
|
|
gptkbp:controls
|
elevators
ailerons
rudder
|
|
gptkbp:countryOfOrigin
|
gptkb:France
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Henri_Farman
1920s
|
|
gptkbp:enginePower
|
450 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1930
1930-06-01
|
|
gptkbp:fuelCapacity
|
800 L
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:height
|
4.0 m
|
|
gptkbp:historicalSignificance
|
early airliner development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Farman F.3902
|
|
gptkbp:influenced
|
later transport aircraft designs
|
|
gptkbp:influencedBy
|
Farman F.60 Goliath
|
|
gptkbp:landingGear
|
tailwheel
|
|
gptkbp:length
|
15.0 m
|
|
gptkbp:manufacturer
|
gptkb:Farman_Aviation_Works
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
3000 kg
|
|
gptkbp:notableFeature
|
high wing configuration
|
|
gptkbp:numberBuilt
|
50
|
|
gptkbp:numberOfEpisodes
|
2
|
|
gptkbp:operationalHistory
|
used in commercial flights
|
|
gptkbp:operationalRole
|
passenger transport
|
|
gptkbp:passengerCapacity
|
10
|
|
gptkbp:productionYears
|
1930-1935
|
|
gptkbp:propulsion
|
variable pitch
|
|
gptkbp:range
|
1000 km
|
|
gptkbp:relatedAircraft
|
gptkb:Farman_F.3910
gptkb:Farman_F.3901
|
|
gptkbp:retirementYear
|
1940
|
|
gptkbp:role
|
civil aviation
transport aircraft
|
|
gptkbp:services
|
1930-1940
4000 m
|
|
gptkbp:successor
|
gptkb:Farman_F.3910
|
|
gptkbp:usedBy
|
gptkb:French_Air_Force
|
|
gptkbp:variant
|
gptkb:Farman_F.3901
|
|
gptkbp:wingArea
|
60 m²
|
|
gptkbp:wingspan
|
20.0 m
|