CANSA C.6

__NOTOC__ Infobox Aircraft
name=C.6 Falchetto


caption=
type=Military trainer
manufacturer=CANSA
designer=Giacomo Mosso and Isidoro Martignago
first flight=30 June 1941
introduced=
retired=
status=
primary user=
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produced=
number built=2
variants with their own articles=

The CANSA C.6 was a training biplane developed in Italy during World War II. It was intended as an aerobatic intermediate trainer for the Regia Aeronautica and was of conventional tailskid configuration with a single-bay wing cellule with swept outer panels. Two prototypes were constructed, the single-seat C.6 and the two-seat C.6B, but no production order ensued.

pecifications (C.6B)

aerospecs
met or eng?= met

crew=Two, pilot and instructor
capacity=
length m=7.83
length ft=25
length in=8
span m=8.65
span ft=28
span in=4
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=3.10
height ft=10
height in=2
wing area sqm=21.7
wing area sqft=233
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=930
empty weight lb=2,050
gross weight kg=1,255
gross weight lb=2,767
lift kg=
lift lb=

eng1 number=1
eng1 type=Isotta-Fraschini Beta RC.10
eng1 kw= 209
eng1 hp= 280
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
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eng2 kw=
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max speed kmh=162
max speed mph=260
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=1,150
range miles=717
endurance h=
endurance min=
ceiling m=6,500
ceiling ft=21,320
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=
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armament6=

References

*
*
* [http://www.aerei-italiani.net/SchedeT/aereocansac6.htm aerei-italiani.net]

ee also

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