Wibault 210
Avions Michel Wibault · France · first flew 1929 · fighter
A French single-engine, single-seat low-wing monoplane fighter of the late 1920s.
Recognition (WEFT)
| W — Wings | Low-mounted, tapered |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 6.87 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Single-seat low-wing monoplane
- Water-cooled V-12 Hispano-Suiza engine
- Single engine of 500 hp
A low-wing monoplane fighter with a water-cooled Hispano-Suiza V-12.
Specifications
- The Wibault 210 has a length of 6.87 m (23 ft).
- It has a wingspan of 9.4 m (31 ft).
- Its maximum speed is 300 km/h (186 mph).
- Typical crew: 1.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
Designed by Michel Wibault, it first flew in late April 1929.
Variants
Two examples of the Wib 210 were built.
Where you'll see it
Flight tests revealed vibration problems and development was quickly abandoned.
Related aircraft
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