Patent ID: 7950604

Claim:
An engine attachment pylon for an aircraft, comprising: an assembly of an upper spar, a lower spar, first and second lateral panels, and transverse ribs connecting the spars and panels; and an aft engine attachment fitted with an aft attachment body, wherein the aft engine attachment includes first and second lateral brackets, each of the first and second lateral brackets includes a longitudinal portion which extends in a longitudinal direction of the pylon and a transverse portion which extends in a transverse direction of the pylon, wherein an outer face of the longitudinal portion of the first and second lateral brackets each contacts an inner face of the first and second lateral panels, respectively, in the transverse direction of the pylon and the longitudinal portion of the first and second lateral brackets each is mounted fixed on the inner face of the first and second lateral panels, respectively, wherein the transverse portion of the first and second lateral brackets each includes an attachment interface for the aft attachment body and the transverse portion of the first and second lateral brackets each passes through a recess formed on the first and second lateral panels, respectively, and wherein the transverse portions of the first and second lateral brackets extend in the transverse direction of the pylon beyond the first and second lateral panels, respectively.