Boisavia Mercurey

Boisavia Mercurey

__NOTOC__ Infobox Aircraft
name=B.60 Mercurey


caption=
type=Civil utility aircraft
manufacturer=Boisavia
designer=
first flight=3 April 1949
introduced=
retired=
status=
primary user=
more users=
produced=
number built=46
variants with their own articles=
The Boisavia B.60 Mercurey was a four-seat light aircraft developed in France shortly after World War II. It 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 Renault 4Pei engine
* B.601 Mercurey - Powered by a 190-hp (142-kW) Avco Lycoming O-435-A engine (3 built)
** B.601L Mercurey - Main production version, equipped with an Avco Lycoming O-360-A engine (27 built)
* B.602 Mercurey - Powered by a 165-hp (123-kW) Continental E-165-4 engine (2 built)
* B.603 Mercurey Special - Glider tug version, powered by a 240-hp (179-kW) Argus As 10 engine (5 built)
* B.604 Mercurey II - Dedicated glider tug with lengthened fuselage, powered by a 230-hp (172-kW) Salmson 9ABC radial piston engine (1 built)
* B.605 Mercurey - Similar to the B.60 Mercury, powered by a 170-hp (127-kW) Regnier 4L-O2 engine (4 built)
* B.606 Mercurey - Regnier 4L-O0 engine (1 built)

pecifications (B.60)

aerospecs
met or eng?= met

crew=one pilot
capacity=3 passengers
length m=7.09
length ft=23
length in=3
span m=11.38
span ft=37
span in=4
dia m=
dia ft=
dia in=
height m=2.08
height ft=6
height in=10
wing area sqm=18.0
wing area sqft=194
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=520
empty weight lb=1,146
gross weight kg=1,000
gross weight lb=2,205

eng1 number=1
eng1 type=Renault 4Pei
eng1 kw= 104
eng1 hp= 140
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=

max speed kmh=235
max speed mph=146
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=1,100
range miles=684
endurance h=
endurance min=
ceiling m=5,500
ceiling ft=18,045
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
armament2=
armament3=
armament4=
armament5=
armament6=

References

*
*
*

ee also

aircontent

related=

similar aircraft=

sequence=
* B.50 - B.60 - B.80 - B.260

lists=

see also=


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