|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
civil aviation
cantilever wing
|
|
gptkbp:avionics
|
analog
|
|
gptkbp:cockpit
|
pressurized
|
|
gptkbp:constructionMaterial
|
metal
|
|
gptkbp:controls
|
elevator
rudder
aileron
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Henri_Farman
high-wing configuration
|
|
gptkbp:emergencyServices
|
yes
|
|
gptkbp:enginePower
|
300 hp
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:firstFlight
|
1950
|
|
gptkbp:fuelCapacity
|
2000 L
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
6.0 m
|
|
gptkbp:historicalSignificance
|
post-war transport aircraft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Farman F.2201A
|
|
gptkbp:influencedBy
|
gptkb:Farman_F.2200
|
|
gptkbp:interiorFeatures
|
single aisle
|
|
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:missions
|
manual
|
|
gptkbp:nationality
|
gptkb:France
|
|
gptkbp:numberOfEpisodes
|
2
|
|
gptkbp:operationalHistory
|
used in various airlines.
|
|
gptkbp:passengerCapacity
|
1
20
2000 kg
|
|
gptkbp:primaryUser
|
gptkb:French_Air_Force
|
|
gptkbp:productionYears
|
1950-1955
|
|
gptkbp:propulsion
|
variable-pitch
|
|
gptkbp:range
|
1500 km
|
|
gptkbp:relatedAircraft
|
Farman F.2202
|
|
gptkbp:retirementYear
|
1965
|
|
gptkbp:role
|
transport aircraft
|
|
gptkbp:seatingCapacity
|
2-2 configuration
|
|
gptkbp:services
|
6000 m
1951-1965
|
|
gptkbp:successor
|
none
|
|
gptkbp:totalGoals
|
50
|
|
gptkbp:variant
|
gptkb:Farman_F.2201B
|
|
gptkbp:wingArea
|
100 m²
|
|
gptkbp:wingspan
|
30.0 m
|
|
gptkbp:yearEstablished
|
1951
|