Английская Википедия:AIDC XC-2

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Шаблон:Short description

Шаблон:Infobox Aircraft Type

The AIDC XC-2 was a prototype civil transport aircraft designed in the 1970s in Taiwan. 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.

Specifications (performance estimated)

Шаблон:Aircraft specs

See also

Шаблон:Aircontent

References

Шаблон:Reflist

Further reading

External links

Шаблон:Commons category

Шаблон:AIDC aircraft