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#1760

Aérospatiale Alouette III

🇫🇷 France ·first flew 1959· light utility helicopter

🚁 helicopter turboshaft ✓ still flying
Aérospatiale Alouette III, photo 1 of 9
1/9 Gordon Zammit· GFDL 1.2

what is it?

The Aérospatiale Alouette III (French pronunciation: [alwɛt], Lark; company designations SA 316 and SA 319) is a single-engine, light utility helicopter developed by French aircraft company Sud Aviation. Introduced in the early 1960s, more than 2,000 units were built during its production run that extended for six decades. The Alouette III was developed as an enlarged derivative of the earlier successful Alouette II. It shared many design elements with its predecessor while offering an extra pair of seats and other refinements.

How to recognise it: 1 turboshaft engine · 11 m main rotor

base stats

  • speed 210 km/htop speed
  • range 540 kmwithout refuelling
  • seats 5passengers
  • size 2,200 kgmax take-off weight
  • built 2,000made in total

Bars compare against all aircraft: 3,500 km/h, 20,000 km, 850 seats; size and number built on a log scale up to 640 t (An-225) and 45,000 built (Cessna 172).

fun facts

  • First flew 67 years ago, in 1959.
  • Top speed is 1.6× a car on the Dutch motorway (130 km/h).
  • Rotor of 11 m: about 2 cars parked nose to tail.

turboshaft: A turbine that turns a shaft, usually a helicopter rotor.

spec sheet

first flight
1959-02-28
introduced
1960
retired
2004
status
still flying
number built
2,000
role
light utility helicopter
origin
🇫🇷 France
makers
Saab Group, Aérospatiale, Sud-Aviation
engines
1× Turbomeca Artouste IIIB
crew
2
passengers
5
length
10 m
rotor diameter
11 m
height
3 m
max take-off weight
2,200 kg
top speed
210 km/h
cruise speed
185 km/h
range
540 km
ceiling
3,200 m

Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.

Sources: Wikidata Q181251, Wikipedia: Aérospatiale Alouette III (CC BY-SA 4.0).Updated 2026-10-24.

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