gptkbp:instance_of
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gptkb:helicopter
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gptkbp:aircraft_configuration
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single main rotor, tail rotor
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gptkbp:aircraft_operated
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gptkb:civil_aviation
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gptkbp:aircraft_type
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light helicopter
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gptkbp:avionics
|
modern avionics suite
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gptkbp:cargo_capacity
|
1,200 kg
1,000 kg
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gptkbp:ceiling
|
5,500 m
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gptkbp:certification
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gptkb:EASA
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gptkbp:crew
|
1-2
1-2 pilots
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gptkbp:design
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gptkb:Aerospatiale
twin-engine
multi-role helicopter
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gptkbp:diameter
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gptkb:Fenestron
11.0 m
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gptkbp:engine_power
|
2 x 350 hp
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gptkbp:engine_type
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gptkb:turbofan_engine
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gptkbp:first_flight
|
gptkb:1980
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gptkbp:fuel_capacity
|
600 L
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gptkbp:fuselage_material
|
aluminum alloy
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gptkbp:height
|
3.3 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
AS355 Écureuil II
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gptkbp:introduced
|
gptkb:1980
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gptkbp:landing_distance
|
1,000 m
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gptkbp:length
|
13.3 m
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gptkbp:manufacturer
|
gptkb:Eurocopter
|
gptkbp:market_segment
|
commercial and private use
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gptkbp:max_speed
|
240 km/h
260 km/h
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gptkbp:max_takeoff_weight
|
2,500 kg
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gptkbp:military_technology
|
AS355 F, AS355 F2
AS355 N, AS355 P
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gptkbp:notable_features
|
quiet operation
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gptkbp:notable_operators
|
gptkb:Airbus
|
gptkbp:number_built
|
over 1,000
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gptkbp:number_of_engines
|
2
|
gptkbp:operational_history
|
used in various roles globally
|
gptkbp:passenger_capacity
|
5-6
|
gptkbp:payload_capacity
|
1,200 kg
|
gptkbp:primary_use
|
gptkb:transportation
|
gptkbp:production_location
|
gptkb:France
|
gptkbp:production_years
|
1980-present
|
gptkbp:propulsion
|
turbine engines
|
gptkbp:range
|
600 km
|
gptkbp:related_model
|
AS350, AS355 N
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gptkbp:role
|
gptkb:helicopter
|
gptkbp:safety_features
|
dual hydraulic systems
|
gptkbp:service_ceiling
|
5,500 m
|
gptkbp:service_entry
|
gptkb:1980
|
gptkbp:status
|
in production
|
gptkbp:takeoff_distance
|
1,200 m
|
gptkbp:variant
|
gptkb:AS350_Écureuil
|
gptkbp:weight
|
1,400 kg
|
gptkbp:wingspan
|
not applicable
|
gptkbp:bfsParent
|
gptkb:AS350_Écureuil
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gptkbp:bfsLayer
|
6
|