Alouette II SA 319B

GPTKB entity

Properties (54)
Predicate Object
gptkbp:instanceOf gptkb:helicopter
gptkbp:aircraft light helicopter
gptkbp:airlines 1 pilot
gptkbp:armament machine guns
gptkbp:avionics basic navigation equipment
gptkbp:constructionMaterial metal construction
metal and composite materials
gptkbp:countryOfOrigin gptkb:France
gptkbp:crew 1
gptkbp:design Sud Aviation
single rotor
gptkbp:discontinued 1980s
gptkbp:engine gptkb:Turbomeca_Artouste_II
gptkbp:firstFlight 1955
gptkbp:fuelCapacity 400 L
gptkbp:headlights gptkb:fenestron
conventional tail
gptkbp:height 3.2 m
https://www.w3.org/2000/01/rdf-schema#label Alouette II SA 319B
gptkbp:introduced 1956
gptkbp:legacy influenced future helicopter designs
gptkbp:length 12.5 m
gptkbp:manufacturer Sud Aviation
gptkbp:maximumDepth 1,000 kg
gptkbp:maxSpeed 210 km/h
gptkbp:maxTakeoffWeight 2,200 kg
gptkbp:militaryRank charter services
transport missions
gptkbp:modifications various upgrades
gptkbp:notableUsers gptkb:French_Army
gptkbp:numberBuilt 1,500
gptkbp:operationalRange 300 km
gptkbp:participatesIn reconnaissance
air ambulance
gptkbp:passengerCapacity 3
500 kg
gptkbp:powers 560 hp
gptkbp:produces 1955-1980
gptkbp:propulsion turbine engine
gptkbp:range 600 km
gptkbp:retired 1980s
gptkbp:role utility helicopter
gptkbp:rotorDiameter two-blade rotor
gptkbp:service_ceiling 4,500 m
gptkbp:serviceHistory used in various conflicts
gptkbp:services 1956
4,500 m
gptkbp:successor gptkb:Alouette_III
gptkbp:takeoffDistance 300 m
200 m
gptkbp:usedBy military forces
gptkbp:variant gptkb:SA_319B
gptkbp:weight 1,200 kg
gptkbp:wingspan 11.0 m