Caproni Ca.122

__NOTOC__ Infobox Aircraft
name=Ca.122


caption=
type=Bomber and military transport
manufacturer=Caproni
designer=
first flight=
introduced=
retired=
status=Prototypes only
primary user=
more users=
produced=
number built=
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The Caproni Ca.122 was a prototype bomber and military transport aircraft built in Italy in the mid-1930s. It was a conventional low-wing monoplane with fixed undercarriage. Power was provided by twin Gnome-Rhône 14K radial engines. No production ensued for either this or the a 28-seat airliner version designated Ca.123.

pecifications (Ca.123)

aerospecs
ref=
met or eng?= met

crew=Three: Pilot, co-pilot, and radio operator
capacity=28 passengers
length m=18.19
length ft=59
length in=8
span m=27.87
span ft=91
span in=5
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=6.00
height ft=19
height in=8
wing area sqm=91.6
wing area sqft=986
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=5,300
empty weight lb=11,686
gross weight kg=8,800
gross weight lb=19,404
lift kg=
lift lb=

eng1 number=2
eng1 type=Gnome-Rhône 14K
eng1 kw= 650
eng1 hp= 870
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=
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max speed kmh=340
max speed mph=211
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=1,500
range miles=932
endurance h=
endurance min=
ceiling m=7,530
ceiling ft=27,400
glide ratio=
climb rate ms=0.1
climb rate ftmin=13
sink rate ms=
sink rate ftmin=

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

References

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ee also

aircontent

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similar aircraft=

sequence= ← Ca.119 -
Ca.120 -
Ca.121 - Ca.122 - Ca.123 -
Ca.124 -
Ca.125 -
Ca.126 →

lists=

see also=