The SAB-SEMA 10 was designed by the Societé d'Etudes de Materiel d'Aviation (SEMA) and built by the Société Aérienne Bordelaise (SAB) to compete for a 1933 French government contract for an intermediate and advanced military trainer.

It was a conventional biplane, metal framed and fabric covered, powered by a 240 hp (180 kW) Lorraine 7Mc Mizar seven-cylinder radial engine.

It was then re-engined with a more powerful 300 hp (224 kW) Lorraine 9Na Algol nine-cylinder radial with a Townend ring cowling.

The lower wing had a smaller chord than the upper one but both carried ailerons, externally connected.

The fin was tall and the rudder extended to the bottom of the fuselage, moving between separate elevators.