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Does anyone know the angular deflection limits of the longitudinal (pitch) and lateral (roll) axis of Airbus's side-stick?

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From this site:

enter image description here

So max deflection in pitch is +/- 16 deg, in roll it is +/- 20 deg

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There is a rather quick YouTube video by a gentleman called Capt. Joe which can partially answer your question.

The limits of the effective deflection of the sidestick is presented on the PFD, which that also changes with many variable factors to allow the aircraft to operate within its approved and safe performance envelope.

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    $\begingroup$ What's presented on the PFD is elevator & aileron deflection, not sidestick deflection. $\endgroup$ – Koyovis Nov 23 '17 at 14:18
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    $\begingroup$ And anyway the answer should be in the text, not in the linked video only (or it should be a comment). $\endgroup$ – mins Nov 25 '17 at 9:55
  • $\begingroup$ I tried to put in the link in my comment, but unfortunately the whole YouTube piece popped up as my answer. Sorry for disturbing you, I beg your forgiveness. $\endgroup$ – Hercules-63 Nov 27 '17 at 16:01

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