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gptkbp:instance_of
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gptkb:aircraft
|
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Breguet_No._50
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
3.5 m
passenger transport
2500 kg
civil transport aircraft
Breguet 690
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:aspect_ratio
|
8:1
|
|
gptkbp:cockpit
|
enclosed cockpit
|
|
gptkbp:crew
|
2
1 pilot
|
|
gptkbp:decommissioned
|
gptkb:1940
|
|
gptkbp:design
|
gptkb:Louis_Breguet
|
|
gptkbp:developer
|
Breguet 50 series
|
|
gptkbp:engine
|
gptkb:Gnome_et_Rhône
2
600 hp
|
|
gptkbp:engine_type
|
gptkb:engine
|
|
gptkbp:features
|
low drag design
|
|
gptkbp:first_flight
|
gptkb:1935
|
|
gptkbp:fuel_capacity
|
800 L
|
|
gptkbp:historical_significance
|
used in military transport
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Breguet No. 50 A
|
|
gptkbp:influenced_by
|
gptkb:Breguet_14
|
|
gptkbp:inspiration
|
gptkb:Breguet_19
|
|
gptkbp:introduced
|
1936
|
|
gptkbp:is_used_by
|
gptkb:French_Air_Force
|
|
gptkbp:landing_gear
|
fixed landing gear
|
|
gptkbp:length
|
15.5 m
|
|
gptkbp:manufacturer
|
gptkb:Breguet
|
|
gptkbp:material
|
12.5 m
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
500 m
600 m
3000 kg
|
|
gptkbp:notable_users
|
French military
|
|
gptkbp:number_built
|
50
|
|
gptkbp:operational_history
|
served in World War II
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:production_years
|
1935-1940
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
1000 km
|
|
gptkbp:retirement_year
|
gptkb:1940
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
gptkb:6
|
|
gptkbp:service_ceiling
|
6000 m
|
|
gptkbp:services
|
1936
|
|
gptkbp:setting
|
high-wing monoplane
|
|
gptkbp:successor
|
gptkb:Breguet_761
|
|
gptkbp:variant
|
Breguet 50 A.1
|
|
gptkbp:wing_area
|
50 m²
|
|
gptkbp:wingspan
|
20.0 m
|