Brochet MB.110

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The Brochet MB.110 was a four-seat light aircraft developed in France in the early 1950s. It was a further derivative of the Brochet MB.70 family, but while generally similar to those aircraft, the MB.110 was a substantially new and enlarged design. Apart from a bigger passenger cabin with one more seat than previous models, the wing and tail were redesigned, and a more powerful engine was fitted. Two examples were built.

Specifications

General characteristics

Crew: One pilot
Capacity: 3 passengers
Length: 7.68 m (25 ft 2 in)
Wingspan: 11.06 m (36 ft 3 in)
Height: 2.56 m (8 ft 5 in)
Wing area: 15.7 m² (169 ft²)
Empty weight: 800 kg (1,764 lb)
Gross weight: 1,300 kg (2,866 lb)
Powerplant: 1 × SNECMA-built Regnier 4L-02, 127 kW (170 hp)

Performance

Maximum speed: 240 km/h (150 mph)
Range: 1,000 km (620 miles)

References

Wikimedia Commons has media related to Brochet MB.110.

Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 215.
World Aircraft Information Files. London: Bright Star Publishing. pp. File 890 Sheet 99.
Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. pp. 100–01.

v t e Aircraft designed by Maurice Brochet

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