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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_configuration
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twin-engine configuration
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gptkbp:aircraft_operated
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gptkb:civil_aviation
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gptkbp:capacity
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10 passengers
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gptkbp:cockpit
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enclosed cockpit
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gptkbp:control_surfaces
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elevator, ailerons, rudder
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gptkbp:crew
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2
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gptkbp:decommissioned
|
1940s
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gptkbp:design
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gptkb:Henri_Farman
high-wing monoplane
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gptkbp:engine_power
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450 hp
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gptkbp:engine_type
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piston engine
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gptkbp:first_flight
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gptkb:1929
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gptkbp:fuel_capacity
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800 L
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gptkbp:historical_significance
|
used in early commercial aviation
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|
https://www.w3.org/2000/01/rdf-schema#label
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Farman F.4900
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gptkbp:introduced
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gptkb:1930
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gptkbp:landing_gear
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fixed landing gear
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gptkbp:length
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14.0 m
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gptkbp:manufacturer
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gptkb:Farman_Aviation_Works
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gptkbp:max_speed
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200 km/h
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gptkbp:notable_users
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gptkb:French_Air_Force
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gptkbp:number_built
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50
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gptkbp:number_of_engines
|
2
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gptkbp:passenger_capacity
|
1-2-1 seating arrangement
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gptkbp:production_location
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gptkb:France
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gptkbp:production_years
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1929-1935
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gptkbp:range
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800 km
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gptkbp:retired
|
1940s
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gptkbp:role
|
gptkb:transport_aircraft
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gptkbp:service_ceiling
|
4000 m
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gptkbp:successor
|
Farman F.5100
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gptkbp:tail_type
|
conventional tail
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gptkbp:variant
|
Farman F.4901
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gptkbp:weight
|
2500 kg
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gptkbp:weight_limit
|
4000 kg
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gptkbp:wing_area
|
60 m²
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gptkbp:wingspan
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20.0 m
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gptkbp:bfsParent
|
gptkb:Paul_Farman
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gptkbp:bfsLayer
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6
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