Brochet MB.120
Brochet · France · first flew 1954 · light aircraft
The Brochet MB.120 was a two-seat light aircraft developed in France in the 1950s.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | Wingspan of 10.66 m on a fuselage 6.50 m long |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- High-wing two-seat light aircraft
- Single Continental C90 air-cooled flat-four engine
- Wingspan of 10.66 m on a fuselage 6.50 m long
A two-seat high-wing light aircraft powered by a 90 hp Continental C90 flat-four.
Specifications
- The Brochet MB.120 has a length of 6.5 m (21 ft).
- It has a wingspan of 10.66 m (35 ft).
- Its maximum speed is 195 km/h (121 mph).
- Typical crew: 1.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It was designed by Maurice Brochet and first flew on 5 April 1954.
Variants
Only one example was built.
Where you'll see it
It was a sports plane with a top speed of 195 km/h and a cruising speed of 170 km/h.
Related aircraft
- Brochet MB.110
- Brochet MB.100
- Brochet MB.80
- Brochet MB.50 Pipistrelle
- Ambrosini F.7 Rondone
- Auster AOP.9
- Breguet 901 Mouette
- CAB GY-30 Supercab
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