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I was checking some information about the a340-600 and got this statement: "thickness/ chord ratios 15.25 per cent at root, 11.27 per cent at inner kink, 9.86 per cent at outer kink and 10.60 per cent at tip" I know where the inner kink is but what is the outer kink and where is it located?

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    $\begingroup$ I edited a few things to make your question a little more readable. If I deleted anything important, feel free or roll back the changes. Welcome to Aviation.SE! $\endgroup$
    – dalearn
    Jan 6, 2020 at 20:26

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The outer kink on A340-600 wing is located just outboard of the outboard engine, note trailing edge kink in planform drawing.

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    $\begingroup$ it is not that visible at first glance $\endgroup$ Jan 7, 2020 at 10:51
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    $\begingroup$ @IbrahimJaafar Indeed not, but a straightedge helps ;) $\endgroup$ Jan 7, 2020 at 19:25

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