|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:control_surfaces
|
gptkb:elevator
ailerons
rudder
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Henri_Farman
|
|
gptkbp:engine
|
gptkb:Gnome-Rhône_9_K
|
|
gptkbp:first_flight
|
gptkb:1929
|
|
gptkbp:fuel_capacity
|
300 L
|
|
gptkbp:height
|
4.0 m
|
|
gptkbp:historical_significance
|
early airliner development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Farman F.1000
|
|
gptkbp:influenced
|
subsequent aircraft designs
|
|
gptkbp:influenced_by
|
gptkb:Farman_F.60_Goliath
|
|
gptkbp:inspiration
|
gptkb:military_aircraft
|
|
gptkbp:introduced
|
gptkb:1930
|
|
gptkbp:landing_distance
|
250 m
|
|
gptkbp:landing_gear
|
fixed
|
|
gptkbp:legacy
|
pioneering airliner
|
|
gptkbp:length
|
14.0 m
|
|
gptkbp:manufacturer
|
gptkb:Farman_Aviation_Works
|
|
gptkbp:max_speed
|
200 km/h
|
|
gptkbp:nationality
|
gptkb:France
|
|
gptkbp:notable_feature
|
robust construction
high wing loading
large passenger capacity
biplane design
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_period
|
1930s
|
|
gptkbp:operational_use
|
commercial aviation
|
|
gptkbp:passenger_capacity
|
gptkb:10
|
|
gptkbp:primary_use
|
passenger transport
|
|
gptkbp:propeller
|
2
|
|
gptkbp:range
|
800 km
|
|
gptkbp:retired
|
gptkb:1935
|
|
gptkbp:role
|
gptkb:transport_aircraft
|
|
gptkbp:service_ceiling
|
4000 m
|
|
gptkbp:successor
|
gptkb:Farman_F.1100
|
|
gptkbp:takeoff_distance
|
300 m
|
|
gptkbp:type
|
gptkb:biplane
|
|
gptkbp:used_by
|
gptkb:French_Air_Force
|
|
gptkbp:variant
|
Farman F.1001
|
|
gptkbp:wing_area
|
60 m²
|
|
gptkbp:wing_configuration
|
gptkb:biplane
|
|
gptkbp:wingspan
|
20.0 m
|
|
gptkbp:bfsParent
|
gptkb:Paul_Farman
|
|
gptkbp:bfsLayer
|
6
|