The method involves supplying a structural arrangement comprising a metal net which is made of metal and is preinpregnated with a resin matrix, where the structural arrangement is laid along different directions with respect to the laminating apparatus. The structural arrangement is laid on a laminating apparatus by a tape-laying machine, where the tape-laying machine is moved along a set of axes by a computer numerical control. The structural arrangement is cured to form a wing section (37).
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