AIDC XC-2

__NOTOC__ Infobox Aircraft
name=XC-2


caption=
type=Civil transport
manufacturer=AIDC
designer=
first flight=1978
introduced=
retired=
status=
primary user=
more users=
produced=
number built=1
variants with their own articles=The AIDC XC-2 was a prototype civil transport aircraft first flown in 1978 in the Republic of China. It was a high-wing monoplane powered by two turboprop engines. The main undercarriage was carried in sponsons on either side of the boxy fuselage, maximising internal space.

The AIDC SC-2 was not selected for production.

pecifications

aerospecs
met or eng?= met

crew=two pilots
capacity=38 passengers "or" 3,850 kg (8,500 lb) of cargo
length m=20.1
length ft=65
length in=11
span m=24.6
span ft=80
span in=8
dia m=
dia ft=
dia in=
height m=7.72
height ft=25
height in=4
wing area sqm=
wing area sqft=
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=12,500
gross weight lb=27,500

eng1 number=2
eng1 type=Lycoming T53-L-701A turboprops
eng1 kw= 1,080
eng1 hp= 1,450
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=425
max speed mph=265
range km=2,130
range miles=1,330
endurance h=
ceiling m=8,500
ceiling ft=27,900
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

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

References

*
* [http://www.luftfahrt-archiv.de/Flugzeugtypen.asp?Type=Link&ID=T1333&Name=XC-2&SID=384204425 luftfahrt-archiv.de]