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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_763_Deux-Ponts
gptkb:Louis_Breguet
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gptkbp:aircraft_operated
|
gptkb:aircraft
logistics support
fixed-wing aircraft
metallic structure
twin-engine
8,000 kg
high-wing
influenced future transport aircraft designs
good short takeoff and landing capabilities
Breguet 941 B
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|
gptkbp:aspect_ratio
|
8:1
|
|
gptkbp:avionics
|
analog instruments
|
|
gptkbp:combat_role
|
transport and logistics
|
|
gptkbp:crew
|
2
|
|
gptkbp:decommissioned
|
gptkb:1975
|
|
gptkbp:design
|
gptkb:Henri_Coandă
|
|
gptkbp:emergency_services
|
2
|
|
gptkbp:engine
|
2
1,200 hp
|
|
gptkbp:engine_type
|
turboprop
Pratt & Whitney Canada P T6
|
|
gptkbp:features
|
large cargo hold
|
|
gptkbp:first_flight
|
gptkb:1958
|
|
gptkbp:first_released
|
gptkb:1960
|
|
gptkbp:fuel_capacity
|
3,000 L
|
|
gptkbp:height
|
8.5 m
|
|
gptkbp:historical_significance
|
used in various military operations
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Breguet 941
|
|
gptkbp:interior_features
|
passenger and cargo
|
|
gptkbp:involved_units
|
gptkb:30
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
22.5 m
|
|
gptkbp:manufacturer
|
gptkb:Breguet
|
|
gptkbp:material
|
monocoque
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
600 m
800 m
12,000 kg
|
|
gptkbp:notable_features
|
high-wing design
|
|
gptkbp:notable_users
|
gptkb:French_Navy
|
|
gptkbp:operational_range
|
1,200 km
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:primary_user
|
gptkb:French_Air_Force
|
|
gptkbp:production_years
|
1958-1960
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirement_year
|
gptkb:1970
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
gptkb:30
5,000 kg
rear ramp
|
|
gptkbp:service_ceiling
|
7,500 m
|
|
gptkbp:service_history
|
operated in various countries
|
|
gptkbp:successor
|
Breguet 941 B
|
|
gptkbp:surface
|
elevators and ailerons
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:wing_area
|
70 m²
|
|
gptkbp:wingspan
|
25.5 m
|