| 词条 | AIDC XC-2 | ||||||||||||||||
| 释义 |
The AIDC XC-2 was a prototype civil transport aircraft first flown in 1978 in Taiwan (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. A single prototype was built and was not selected for production. A scale model of the XC-2 is found at Hualien Air Force Base. Specifications{{aerospecs|met or eng?=met |ref=Jane's All The World's Aircraft 1980-81 [1] |crew=two pilots |capacity=38 passengers or {{cvt|3850|kg}} of cargo |length m=20.10 |length ft=65 |length in=11¼ |span m=24.90 |span ft=80 |span in=8⅜ |height m=7.72 |height ft=25 |height in=4 |wing area sqm=65.4 |wing area sqft=704 |aspect ratio= |empty weight kg=7,031 |empty weight lb=15,500 |gross weight kg=12,474 |gross weight lb=27,500 |eng1 number=2 |eng1 type=Lycoming T53-L-701A turboprops |eng1 kw=1,082 |eng1 hp=1,451 |max speed kmh=392 |max speed mph=244 |cruise speed kmh=333 |cruise speed mph=207[2] |range km=1,661 |range miles=1,032 |endurance h= |ceiling m=8,015 |ceiling ft=26,300 |climb rate ms=7.6 |climb rate ftmin=1500 }} See also{{aircontent||related= |similar aircraft=
}} References1. ^{{cite book |title=Jane's All The World's Aircraft 1980-81 |last=Taylor|first= John W.R. (ed.)| |year=1980 |publisher= Jane's Publishing|location=London |isbn= 0-7106-0705-9 |pages=177-178}} 2. ^econ. cruise Further reading
External links{{commons category|AIDC XC-2}}
6 : AIDC aircraft|Republic of China airliners 1970–1979|High-wing aircraft|Abandoned civil aircraft projects|Aircraft first flown in 1978|Twin-turboprop tractor aircraft |
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