Aviasud Mistral
Aviasud · France · first flew 1985 · light aircraft
The Aviasud Mistral is a French ultralight two-seat aircraft of all-composite construction, designed for the light aviation market and first flown in 1985. Its clean aerodynamic form and side-by-side seating made it popular among sport pilots.
Recognition (WEFT)
| W — Wings | Low-mounted, tapered |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 5.66 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- French ultralight two-seat side-by-side low-wing monoplane
- All-composite construction with distinctive bubble canopy
- Compact dimensions suited to microlight regulations
Recognizable by its sleek composite fuselage, low wing with slight taper, bubble canopy, and very small overall dimensions characteristic of French ultralights.
Specifications
- The Aviasud Mistral has a length of 5.66 m (19 ft).
- It has a wingspan of 9.4 m (31 ft).
- Its maximum speed is 155 km/h (96 mph).
- Typical crew: 1-2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
Designed and built by Aviasud Ingénierie in France, the Mistral entered the market at a time of growing interest in composite ultralight aircraft. It was offered in kit form and as a factory-built aircraft.
Variants
Several variants were produced with different engine options and minor airframe refinements to meet evolving microlight certification standards.
Where you'll see it
Operated widely across France and Europe by private owners and flying clubs as a sport and training aircraft.
Related aircraft
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