An assembly for an aircraft including a wing element, a suspension pylon, a mechanism of attaching the pylon onto the element, including two forward half-attachments, each including a shackle and configured to resist forces applied along a vertical direction. The shackle is mounted firstly articulated onto a first fitting fixed to a forward spar of the element extending along the direction of the width, and is secondly mounted articulated onto a second fitting fixed to the rigid structure of the pylon. The two shackles are arranged in the same plane parallel to the direction of the width.
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