Single-engine pistongeneral aviation utility aircraft
B.60 Mercurey
The Boisavia B.60 Mercurey was a series of four-seat light aircraft developed in France shortly after World War II.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Société Boisavia
- Category
- Single-engine piston
- Country of origin
- France
- First flight
- 1949-04-03
Specifications
- Cruise speed
- 110 kt
- Max speed
- 127 kt
- Range
- 650 nm
- Service ceiling
- 18,000 ft
- Rate of climb
- 790 ft/min
- Max takeoff weight
- 2,815 lb
- Empty weight
- 1,565 lb
- Fuel capacity
- 58.1 US gal
- Powerplant
- Lycoming O-320
- Engines
- 1
- Seats
- 4
- Length
- 23 ft
- Wingspan
- 37 ft
- Height
- 7 ft
- Number built
- 46
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.