An aircraft engine attachment pylon including a box formed by an assembly of a first spar, a second spar, two lateral panels, and an aft engine attachment fitted with an aft attachment body. The engine attachment may be provided with two lateral fittings associated with the two lateral panels to which they are fixed to and project from laterally outside the box, each of the fittings forming a plane attachment interface with the attachment body through which bolts pass. Each attachment interface may be in the shape of a straight segment inclined at 45.degree. from a vertical direction of the pylon.
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