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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 XC-2 was not selected for production.

Made by Aerospace Industrial Development Corporation.

Empty Weight Lb
15500
Wing Area Sqm
65
Eng 1 Type
Lycoming T53-L-701A turboprops
Max Speed Mph
244
Cruise Speed Kmh
333
Ceiling Ft
26300
Cruise Speed Mph
207
Eng 1 Kw
1082
Span In
8
Gross Weight Lb
27500
Capacity
38
Number Built
1
Crew
two pilots
Climb Rate Ftmin
1500
Empty Weight Kg
7031
Gross Weight Kg
12474
Height In
4
Range Km
1661
Climb Rate Ms
8
Manufacturer
Aerospace Industrial Development Corporation
Range Miles
1032
First Flight
1978
Max Speed Kmh
392
Height Ft
25
Span Ft
80
Wing Area Sqft
704
Met Or Eng
met
Span M
25
Length Ft
65
Height M
8
Ceiling M
8015
Eng 1 Hp
1451
Eng 1 Number
2
Length In
11
Length M
20
Category
AIDC aircraft
Cancelled aircraft projects
Taiwanese airliners

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