AS355 Écureuil II

GPTKB entity

Statements (57)
Predicate Object
gptkbp:instance_of gptkb:helicopter
gptkbp:aircraft_configuration single main rotor, tail rotor
gptkbp:aircraft_operated gptkb:civil_aviation
gptkbp:aircraft_type light helicopter
gptkbp:avionics modern avionics suite
gptkbp:cargo_capacity 1,200 kg
1,000 kg
gptkbp:ceiling 5,500 m
gptkbp:certification gptkb:EASA
gptkbp:crew 1-2
1-2 pilots
gptkbp:design gptkb:Aerospatiale
twin-engine
multi-role helicopter
gptkbp:diameter gptkb:Fenestron
11.0 m
gptkbp:engine_power 2 x 350 hp
gptkbp:engine_type gptkb:turbofan_engine
gptkbp:first_flight gptkb:1980
gptkbp:fuel_capacity 600 L
gptkbp:fuselage_material aluminum alloy
gptkbp:height 3.3 m
https://www.w3.org/2000/01/rdf-schema#label AS355 Écureuil II
gptkbp:introduced gptkb:1980
gptkbp:landing_distance 1,000 m
gptkbp:length 13.3 m
gptkbp:manufacturer gptkb:Eurocopter
gptkbp:market_segment commercial and private use
gptkbp:max_speed 240 km/h
260 km/h
gptkbp:max_takeoff_weight 2,500 kg
gptkbp:military_technology AS355 F, AS355 F2
AS355 N, AS355 P
gptkbp:notable_features quiet operation
gptkbp:notable_operators gptkb:Airbus
gptkbp:number_built over 1,000
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
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
gptkbp:bfsLayer 6