Brochet MB.110

The Brochet MB.110 was a four-seat light aircraft developed in France in the early 1950s.

MB.110
The prototype Brochet MB.110 at Chavenay airfield near Paris in 1957
Role Sports plane
Manufacturer Brochet
Designer Maurice Brochet
First flight 12 March 1956
Number built 2

Design and development

A further derivative of the Brochet MB.70 family, 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. The prototype aircraft first flew at Chavenay-Villepreux airfield near Paris on 12 March 1956.


Specifications

Data from Jane's All the World's Aircraft 1956–57[1]

General characteristics

  • Crew: 1
  • 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: 15.65 m2 (168.5 sq ft)
  • Aspect ratio: 7.8:1
  • Airfoil: Göttingen 634
  • Empty weight: 800 kg (1,764 lb)
  • Gross weight: 1,300 kg (2,866 lb)
  • Powerplant: 1 × SNECMA-built Regnier 4L air-cooled four-cylinder inline engine, 130 kW (170 hp)
  • Propellers: 2-bladed Ratier-Figeac fixed-pitch propeller

Performance

  • Maximum speed: 240 km/h (150 mph, 130 kn)
  • Cruise speed: 200 km/h (120 mph, 110 kn)
  • Range: 1,600 km (1,000 mi, 870 nmi)
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References
  1. Bridgman 1956, p. 132
  • Bridgman, Leonard (1956). Jane's All The World's Aircraft 1956–57. New York: McGraw-Hill Book Company.CS1 maint: ref=harv (link)
  • Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing. pp. 100–01.
  • 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.

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