Assembly of an attachment pylon with an aircraft engine

An assembly of an attachment pylon with an aircraft engine, the attachment pylon comprising a primary structure comprising an upper spar, a lower spar, port and starboard lateral panels and a front transverse reinforcement, the assembly having a vertical mid-plane and comprising:

• a front engine mount fastened to the attachment pylon and to a casing of the engine, and comprising:
• in the vertical mid-plane and on one of the front transverse reinforcement of the attachment pylon and the casing of the engine, a front tang,
• centered on the vertical mid-plane and on the other of the front transverse reinforcement of the attachment pylon and the casing of the engine, a front clevis,
• in the vertical mid-plane and on one of the lower spar of the attachment pylon and the casing of the engine, a lower tang,
• centered on the vertical mid-plane and on the other of the lower spar of the attachment pylon and the casing of the engine, a lower clevis,
• for each port and starboard lateral panel or on the front transverse reinforcement, a first port tang and a first starboard tang extending orthogonally to the vertical mid-plane,
• for the casing of the engine, a second port tang and a second starboard tang,
• at least a first port link and a first starboard link,
• a front pin connecting the front tang and the front clevis,
• a lower pin connecting the lower tang and the lower clevis,
• a first port pin and a first starboard pin connecting the first port tang and the first starboard tang with the first port link and the first starboard link, and,
• a second port pin and a second starboard pin connecting the second port tang and the second starboard tang with the first port link and the first starboard link.