gptkbp:instanceOf
|
aircraft
|
gptkbp:aircraft
|
retired
twin-engine
civil aviation
cantilever wing
|
gptkbp:cockpit
|
pressurized cockpit
|
gptkbp:constructionMaterial
|
monocoque
|
gptkbp:controls
|
elevators
ailerons
rudder
|
gptkbp:countryOfOrigin
|
gptkb:France
|
gptkbp:crew
|
2
|
gptkbp:design
|
gptkb:Henri_Farman
regional transport
|
gptkbp:enginePower
|
300 hp
|
gptkbp:engineType
|
piston engine
|
gptkbp:firstFlight
|
1950
1950-06-01
|
gptkbp:fuelCapacity
|
2000 L
|
gptkbp:headlights
|
T-tail
|
gptkbp:height
|
6.0 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Farman F.3700
|
gptkbp:influenced
|
gptkb:Farman_F.3800
|
gptkbp:influencedBy
|
Farman F.3600
|
gptkbp:landingGear
|
tricycle gear
|
gptkbp:length
|
20.5 m
|
gptkbp:manufacturer
|
gptkb:Farman_Aviation_Works
|
gptkbp:maxSpeed
|
300 km/h
|
gptkbp:maxTakeoffWeight
|
5000 kg
|
gptkbp:notableFeature
|
high-wing design
none reported
|
gptkbp:numberBuilt
|
50
|
gptkbp:numberOfEpisodes
|
2
|
gptkbp:operationalHistory
|
used in commercial flights
|
gptkbp:operationalRole
|
passenger transport
|
gptkbp:passengerCapacity
|
20
2000 kg
|
gptkbp:productionYears
|
1950-1955
|
gptkbp:propulsion
|
variable-pitch propeller
|
gptkbp:range
|
1500 km
|
gptkbp:retirementYear
|
1960
|
gptkbp:role
|
transport aircraft
|
gptkbp:services
|
1950-1960
6000 m
|
gptkbp:successor
|
gptkb:Farman_F.3710
|
gptkbp:usedBy
|
gptkb:French_Air_Force
|
gptkbp:variant
|
gptkb:Farman_F.3701
|
gptkbp:wingArea
|
100 m²
|
gptkbp:wingspan
|
30.0 m
|