Brochet MB.110
From Wikipedia, the free encyclopedia
| MB.110 | |
|---|---|
| Type | Sports plane |
| Manufacturer | Brochet |
| Designed by | Maurice Brochet |
| Maiden flight | 12 March 1956 |
| Number built | 2 |
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.
[edit] 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)
[edit] References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions, 215.
- World Aircraft Information Files. London: Bright Star Publishing, File 890 Sheet 99.
- Simpson, R. W. (1995). Airlife's General Aviation. Shrewsbury: Airlife Publishing, 100-01.
[edit] See also
|
||||||||||||||
