The Brochet MB.120 two-seater light touring monoplane has the airframe of the three-seat MB.100 remodelled as a two-seater, lighter wings, the landing flaps of the MB.80 and a 90 hp Continental C90 engine.
Flown for the first time on 5 April 1954, the MB.120 has a steel-tube fuselage and a spring-steel cantilever undercarriage. The cabin seats two side-by-side and dual controls can be fitted.
Two prototypes were built.
Engine: 90 hp Continental C90
Wingspan: 34 ft 11 in
Length: 21 ft 3.75 in
Height: 6 ft 6.75 in
Empty weight: 1113 lb
Loaded weight: 1686 lb
Max speed: 121 mph
Cruise: 105.6 mph
Ceiling: 16,404 ft
Range: 497 mi
Seats: 2
All Aero 