Brochet MB.110

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

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

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)

References[]

Wikimedia Commons has media related to Brochet MB.110.

• Bridgman, Leonard (1956). Jane's All The World's Aircraft 1956–57. New York: McGraw-Hill Book Company.
• 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.