Wibault 7
Société des Avions Michel Wibault · France · first flew 1924 · fighter
The Wibault 7 was a 1920s French single-seat monoplane fighter designed and built by Société des Avions Michel Wibault.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 7.45 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Braced parasol monoplane wing
- All-metal construction using Wibault's patented system
- Single-seat fighter with a 480 hp Gnome-Rhone 9Ad radial engine
A single-seat fighter with a high braced parasol wing and a nose-mounted radial engine.
Specifications
- The Wibault 7 has a length of 7.45 m (24 ft).
- It has a wingspan of 11 m (36 ft).
- Its maximum speed is 227 km/h (141 mph).
- Typical crew: 1.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
Developed from the Wib.3, it was a high-wing braced parasol monoplane whose main difference was all-metal construction patented by Wibault. The first prototype flew in 1924, followed by two more.
Variants
Variants included the Wib.72, the Wib.73 built for Paraguay, the carrier-capable Wib.74, and the Polish-built Wibault 70C1 with Bristol Jupiter engines.
Where you'll see it
It placed third in the competition behind the Nieuport-Delage NiD 42 and the Gourdou-Leseurre GL.32, but an order for 25 was placed in January 1927, followed by 60 Wib.72 for the Aéronautique Militaire from 1929. Twenty-six were built under licence in England for Chile.
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