Agusta CP-110

__NOTOC__ Infobox Aircraft
name=CP-110

caption=
type=Light cabin monoplane
manufacturer=Agusta
designer=
first flight=1951
introduced=
retired=
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=The Agusta CP-110 was a prototype Italian four-seat light aircraft first flown in 1951. It failed to attract interest from either civil or military operators, although it was evaluated by the Italian Air Force.

pecifications

aerospecs
met or eng?=met

crew=one pilot
capacity=3 passengers
length m=7.3
length ft=23
length in=11
span m=10.6
span ft=34
span in=9
dia m=
dia ft=
dia in=
height m=
height ft=
height in=
wing area sqm=
wing area sqft=
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=1,100
gross weight lb=2,400

eng1 number=1
eng1 type=Alfa Romeo 110-ter piston engine
eng1 kw= 108
eng1 hp= 145
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=275
max speed mph=170
range km=1,000
range miles=620
endurance h=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

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

ee also

aircontent

related=

similar aircraft=

lists=

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Agusta CP-110

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