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#1948

Aérospatiale Gazelle

🇫🇷 France ·first flew 1967· utility helicopter / armed helicopter

🚁 helicopter turboshaft ✓ still flying
Aérospatiale Gazelle, photo 1 of 10
1/10 Jerry Gunner· CC BY 2.0

what is it?

The Aérospatiale Gazelle (company designations SA 340, SA 341 and SA 342) is a five-seat helicopter developed and initially produced by the French aircraft company Sud Aviation, and later by Aérospatiale. It is the first helicopter to feature a fenestron tail instead of a conventional tail rotor, as well as being the first helicopter to be adapted for single-pilot operations under instrument flight rules. The Gazelle was developed during the 1960s as a successor to the Alouette II as well as to meet a French Army requirement for a new lightweight observation helicopter.

How to recognise it: 1 turboshaft engine · 10.5 m main rotor

base stats

  • speed 310 km/htop speed
  • range 361 kmwithout refuelling
  • seats 4passengers
  • size 1,800 kgmax take-off weight
  • built 1,775made 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 59 years ago, in 1967.
  • Top speed is 2.4× a car on the Dutch motorway (130 km/h).
  • Rotor of 10.5 m: about 2 cars parked nose to tail.

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

spec sheet

first flight
1967-04-07
introduced
1973
status
still flying
number built
1,775
role
utility helicopter / armed helicopter
origin
🇫🇷 France
makers
Airbus Helicopters, SOKO, Aérospatiale
engines
1× Turbomeca Astazou IIIA
crew
1
passengers
4
length
12 m
rotor diameter
10.5 m
height
3.2 m
max take-off weight
1,800 kg
top speed
310 km/h
cruise speed
264 km/h
range
361 km
ceiling
5,000 m

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

Sources: Wikidata Q794595, Wikipedia: Aérospatiale Gazelle (CC BY-SA 4.0).Updated 2026-10-24.

stan runge ef9524a source