gptkbp:instanceOf
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gptkb:helicopter
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gptkbp:aircraft
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light helicopter
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gptkbp:airlines
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1 pilot
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gptkbp:armament
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machine guns
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gptkbp:avionics
|
basic navigation equipment
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gptkbp:constructionMaterial
|
metal construction
metal and composite materials
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gptkbp:countryOfOrigin
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gptkb:France
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gptkbp:crew
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1
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gptkbp:design
|
Sud Aviation
single rotor
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gptkbp:discontinued
|
1980s
|
gptkbp:engine
|
gptkb:Turbomeca_Artouste_II
|
gptkbp:firstFlight
|
1955
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gptkbp:fuelCapacity
|
400 L
|
gptkbp:headlights
|
gptkb:fenestron
conventional tail
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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
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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
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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
|