Misplaced Pages

AIDC XC-2: Difference between revisions

Article snapshot taken from[REDACTED] with creative commons attribution-sharealike license. Give it a read and then ask your questions in the chat. We can research this topic together.
Browse history interactively← Previous editNext edit →Content deleted Content addedVisualWikitext
Revision as of 15:38, 6 April 2007 editRlandmann (talk | contribs)Autopatrolled, Administrators54,016 edits Specifications← Previous edit Revision as of 22:56, 20 April 2007 edit undoR1es (talk | contribs)149 edits Related contentNext edit →
Line 107: Line 107:




]
==Related content==
{{aircontent
<!-- include as many lines are appropriate. additional lines/entries with carriage return. -->

|related=<!-- related developments -->

|similar aircraft=<!-- similar or comparable aircraft -->

|sequence=<!-- designation sequence, if appropriate -->

|lists=<!-- related lists -->

|see also=<!-- other relevant information -->

}}

]

Revision as of 22:56, 20 April 2007

Template:Infobox Aircraft 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. No production ensued.






Specifications

General characteristics

  • Crew: two pilots
  • Capacity: 38 passengers or 3,850 kg (8,500 lb) of cargo

Performance

References

  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 44.
  • luftfahrt-archiv.de
Category:
AIDC XC-2: Difference between revisions Add topic