|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:armament
|
none
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:constructionMaterial
|
wood
metal
|
|
gptkbp:controls
|
ailerons
elevator
rudder
|
|
gptkbp:countryOfOrigin
|
gptkb:France
|
|
gptkbp:covers
|
none
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Henri_Farman
civil aviation
|
|
gptkbp:engineType
|
piston engine
|
|
gptkbp:financial_aid
|
longitudinal stability
directional stability
lateral stability
|
|
gptkbp:firstFlight
|
1929
1929-06-01
|
|
gptkbp:fuelCapacity
|
800 L
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:height
|
4.0 m
|
|
gptkbp:historicalSignificance
|
early transport aircraft
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Farman F.1200 A
|
|
gptkbp:landingGear
|
tailwheel
|
|
gptkbp:length
|
15.0 m
|
|
gptkbp:manufacturer
|
gptkb:Farman_Aviation_Works
|
|
gptkbp:maxSpeed
|
200 km/h
|
|
gptkbp:maxTakeoffWeight
|
80 km/h
3000 kg
|
|
gptkbp:numberOfEpisodes
|
2
|
|
gptkbp:passengerCapacity
|
12
|
|
gptkbp:productionYears
|
1929-1935
|
|
gptkbp:propulsion
|
fixed-pitch
|
|
gptkbp:range
|
800 km
|
|
gptkbp:retired
|
1935
|
|
gptkbp:role
|
transport aircraft
|
|
gptkbp:service_ceiling
|
4000 m
|
|
gptkbp:services
|
4000 m
|
|
gptkbp:successor
|
gptkb:Farman_F.2200
|
|
gptkbp:takeoffDistance
|
70 km/h
|
|
gptkbp:usedBy
|
gptkb:French_Air_Force
|
|
gptkbp:variant
|
gptkb:Farman_F.1200
|
|
gptkbp:wingArea
|
60 m²
|
|
gptkbp:wingspan
|
20.0 m
|