Caproni Ca.97

__NOTOC__ Infobox Aircraft
name=Ca.97


caption=
type=Civil utility aircraft
manufacturer=Caproni
designer=
first flight=1927
introduced=
retired=
status=
primary user=
more users=
produced=
number built=13
variants with their own articles=

The Caproni Ca.97 was a civil utility aircraft produced in Italy in the late 1920s and early 1930s. As originally designed, it was a high-wing braced trimotor monoplane of conventional configuration with one engine mounted in the nose and the other two carried in strut-mounted nacelles at the fuselage sides. Examples were also produced with only the nose engine or only the two nacelle-mounted engines.

Variants

* Ca.97 : Civil utility transport aircraft.
* Ca.97 Idro : Twin-float seaplane version.

pecifications, single-engine version

aerospecs
ref=
met or eng?= met

crew=1-2 pilots
capacity=6 passengers
length m=10.70
length ft=35
length in=2
span m=15.95
span ft=52
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=3.35
height ft=11
height in=0
wing area sqm=40.0
wing area sqft=431
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=1,500
empty weight lb=3,307
gross weight kg=2,495
gross weight lb=5,500
lift kg=
lift lb=

eng1 number=1
eng1 type=Bristol Jupiter
eng1 kw= 373
eng1 hp= 500
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=225
max speed mph=140
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=1,000
range miles=620
endurance h=
endurance min=
ceiling m=7,400
ceiling ft=24,280
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

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

References

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ee also

aircontent

related=

similar aircraft=

sequence= ← Ca.94 -
Ca.95 -
Ca.96 -Ca.97 -
Ca.98 -
Ca.99 -
Ca.100 →

lists=

see also=