gptkbp:instanceOf
|
aircraft
|
gptkbp:aircraft
|
fixed-wing aircraft
high-wing monoplane
|
gptkbp:armament
|
none
|
gptkbp:cockpit
|
open cockpit
|
gptkbp:constructionMaterial
|
wood
fabric-covered wood
|
gptkbp:crew
|
2
|
gptkbp:design
|
gptkb:Henri_Farman
1920s
|
gptkbp:engine
|
1
|
gptkbp:engineType
|
radial engine
|
gptkbp:firstFlight
|
1929
|
gptkbp:fuelCapacity
|
500 liters
|
gptkbp:headlights
|
conventional tail
|
gptkbp:height
|
4.5 m
|
gptkbp:historicalContext
|
interwar aviation era
|
gptkbp:historicalSignificance
|
early airliner development
|
https://www.w3.org/2000/01/rdf-schema#label
|
Farman F.1100-2
|
gptkbp:influenced
|
later transport aircraft designs
|
gptkbp:influencedBy
|
Farman F.60 Goliath
|
gptkbp:landingGear
|
fixed landing gear
|
gptkbp:legacy
|
pioneering air transport
|
gptkbp:length
|
15.5 m
|
gptkbp:manufacturer
|
gptkb:Farman_Aviation_Works
|
gptkbp:maxSpeed
|
200 km/h
|
gptkbp:maxTakeoffWeight
|
3,000 kg
|
gptkbp:notableFeature
|
high wing configuration
|
gptkbp:numberBuilt
|
50
|
gptkbp:operationalArea
|
commercial flights
|
gptkbp:passengerCapacity
|
10
|
gptkbp:productionYears
|
1929-1935
|
gptkbp:propulsion
|
two-bladed propeller
|
gptkbp:range
|
1,000 km
|
gptkbp:role
|
civil aviation
transport aircraft
|
gptkbp:services
|
1935
3,000 m
|
gptkbp:successor
|
gptkb:Farman_F.1200
|
gptkbp:takeoffDistance
|
300 m
250 m
|
gptkbp:type
|
biplane
|
gptkbp:usedBy
|
gptkb:French_Air_Force
|
gptkbp:wingArea
|
50 m²
|
gptkbp:wingspan
|
20.0 m
|