Boisavia Mercurey

Last updated
B.60 Mercurey
OO-KLO.jpg
RoleCivil utility aircraft
National originFrance
Manufacturer Boisavia
First flight3 April 1949
Number built46

The Boisavia B.60 Mercurey was a series of four-seat light aircraft developed in France shortly after World War II.

Contents

Design and operations

Boisavia B.601L Mercurey of Omniair at Dijon's Val Suzon airfield in 1965 Boisavia B.601L F-BHTK Dijon 05.08.65 edited-2.jpg
Boisavia B.601L Mercurey of Omniair at Dijon's Val Suzon airfield in 1965

The Mercurey was a conventional high-wing braced monoplane with fixed tailwheel undercarriage. It was built in small numbers and found use in the normal general aviation roles of tourer, trainer, agricultural aircraft, and glider tug.


Variants

B.60 Mercurey
3 prototypes powered by 100 kW (140 hp) Renault 4Pei engine
B.601 Mercurey
Powered by a 140 kW (190 hp) Avco Lycoming O-435-1 engine;three built.
B.601L Mercurey
Main production version, equipped with an 130 kW (180 hp) Avco Lycoming O-360-A engine;twenty-seven built.
B.602 Mercurey
Powered by a 123 kW (165 hp) Continental E165-4 engine;two built.
B.602A
1x 159 kW (213 hp) Continental O-470-11
B.603 Mercurey Special
Glider tug version, powered by a 180 kW (240 hp) Salmson 8 As engine (Argus As 10);five built.
B.604 Mercurey II
Dedicated glider tug with lengthened fuselage, powered by a 170 kW (230 hp) Salmson 9ABc radial piston engine;one built).
B.605 Mercurey
Similar to the B.60, powered by a 130 kW (170 hp) Régnier 4LO2 (SNECMA 4L-02) engine;four built.
B.606 Mercurey
130 kW (170 hp) Régnier 4LO20 (SNECMA 4L-00) engine;one built.


Specifications (B.60)

Data from Jane's All The World's Aircraft 1958–59 [1]

General characteristics

(or 170 hp (127 kW) Lycoming O-340)

Performance

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References

  1. Bridgman, Leonard, ed. (1957). Jane's All the World's Aircraft 1958-59. London: Jane's All the World's Aircraft Publishing Co. Ltd. pp. 142–143.

Further reading