Brochet MB.110

__NOTOC__ Infobox Aircraft
name=MB.110


caption=
type=Sports plane
manufacturer=Brochet
designer=Maurice Brochet
first flight=12 March 1956
introduced=
retired=
status=
primary user=
more users=
produced=
number built=2
variants with their own articles=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.

pecifications

aerospecs
met or eng?= met

crew=One pilot
capacity=3 passengers
length m=7.68
length ft=25
length in=2
span m=11.06
span ft=36
span in=3
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=2.56
height ft=8
height in=5
wing area sqm=15.7
wing area sqft=169
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=800
empty weight lb=1,764
gross weight kg=1,300
gross weight lb=2,866
lift kg=
lift lb=

eng1 number=1
eng1 type=SNECMA-built Regnier 4L-02
eng1 kw= 127
eng1 hp= 170
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
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eng2 kw=
eng2 hp=
eng2 kn=
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max speed kmh=240
max speed mph=150
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=1,000
range miles=620
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
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armament1=
armament2=
armament3=
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armament5=
armament6=

References

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ee also

aircontent

related=

similar aircraft=

sequence=
* ← MB.70 - MB.80 - MB.100 - MB.110 - MB.120

lists=

see also=