The Wib 210 was designed in response to a 1928 Service Technique de l'Aéronautique (S.T.Aé, Technical Department of Aeronautics) single-seat fighter (C.1) programme.

[1] Like earlier Wibault designs, the Wib 210 was an all-metal aircraft with a largely Duralumin structure and clad with narrow aluminium strips applied longitudinally.

[1] The fuselage was flat sided with rounded decking; the single open cockpit was situated just ahead of the wing trailing edge.

The Wib 210 was armed with a pair of 7.7 mm (0.303 in) synchronised machine guns firing through the propeller arc.

Its flight reports were not encouraging and vibration remained an issue when speeds greater than 350 km/h (217 mph) were reached in shallow dives.