Salmson-Béchereau SB-2

The Salmson-Béchereau SB-2 was a 1923 mid-wing trainer aircraft built by the French company Salmson.

The SB-2 was basically a mid-wing monoplane design. Only one aircraft was built.

The SB-2 was developed into the Salmson-Béchereau SB-3.

SB-2
Engine: 1 x Salmson 1 9AC, 120 hp / 89 kW
Propeller: 2-bladed
Wingspan 7.00m (23 ft 0 in)
Wing area: 11 m2 (120 sq ft)
Length: 6.03 m (19 ft 9 in)
Height: 2.14 m (7 ft 0 in)
Empty weight: 622 kg (1,371 lb)
Maximum speed: 220 km/h (140 mph, 120 kn)
Seats: 1

Saint-Hubert 135 B.O.

A Belgian touring plane, the Saint-Hubert 135 B.O. low-wing monoplane, constructed by the Saint-Hubert Aircraft Engineering Works and designed by Mr. Pierre Baudoux (of Brussels University) and Mr. J. Orta, of the Saint-Hubert Aerodrome. It is equipped with a “Cirrus-Hermes IV” engine, and has a maximum speed of 152 mph and a cruising speed of 127 mph.