- 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 4P ei engine
* B.601 Mercurey - Powered by a 190-hp (142-kW) AvcoLycoming O-435 -A engine (3 built)
** B.601L Mercurey - Main production version, equipped with an AvcoLycoming 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 9A BC 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?= metcrew=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=2,205eng1 number=1
eng1 type=Renault 4P ei
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.260lists=
see also=
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