Aérospatiale SA 315 Lama

E250384

The Aérospatiale SA 315 Lama is a light utility helicopter renowned for its exceptional high-altitude performance, widely used for mountain rescue, transport, and observation missions.

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All labels observed (2)

Label Occurrences
Aérospatiale SA 315 Lama canonical 1
Aérospatiale SA 315B Lama 1

Statements (47)

Predicate Object
instanceOf light utility helicopter
single‑engine helicopter
category civil utility helicopter
military utility helicopter
countryOfOrigin France
crew 1
cruiseSpeed 192 km/h
derivedFrom Aérospatiale Alouette II
Aérospatiale Alouette III
emptyWeight 1020 kg
engineModel Turbomeca Artouste IIIB
engineType turboshaft
firstFlight 1969-03-17
height 3.09 m
ICAOTypeDesignator LAMA
introduced 1971
landingGearType skid landing gear
length 10.24 m
mainRotorBlades 3
mainRotorDiameter 11.02 m
manufacturer Aérospatiale
Aérospatiale
surface form: Sud Aviation
maximumSpeed 228 km/h
maximumTakeoffWeight 1950 kg
notableFeature exceptional high‑altitude performance
notableUse aerial observation missions
high‑altitude transport missions
mountain rescue operations
numberOfEngines 1
passengerCapacity 4
powerplantOutput ~550 shp
primaryConstructionMaterial metal airframe with open‑truss tail boom
productionStart 1971
range 515 km
role mountain rescue helicopter
observation helicopter
transport helicopter
utility helicopter
serviceCeiling 7600 m
status in service
tailRotorBlades 3
usedBy Brazilian Air Force
French Army Light Aviation
Indian Air Force
Indian Army
Royal Nepalese Army
surface form: Nepalese Army

Swiss Air Force

Referenced by (2)

Full triples — surface form annotated when it differs from this entity's canonical label.

Aérospatiale majorProduct Aérospatiale SA 315 Lama
Turbomeca Astazou usedOnAircraft Aérospatiale SA 315 Lama
this entity surface form: Aérospatiale SA 315B Lama