Front engine attachment system for an aircraft engine, having a beam made in three parts

A front engine attachment system configured to fix an engine of an aircraft, the front engine attachment system having:

• an engine pylon having, in its front part, a frontal part having an attachment wall that has a front face, and
• a front engine attachment having a beam, which is fastened to the front face and to which a link rod is fastened on either side of a median plane,
• wherein each link rod is fastened to the beam in an articulated manner by at least one first connection point and is configured to be fastened to the engine in an articulated manner by at least one second connection point,
• wherein the beam is made up of a front plate, an intermediate plate and a rear plate,
• wherein the rear plate is pressed against the front face,
• wherein the front plate is disposed in front of the rear plate, and
• wherein the intermediate plate is disposed between the front plate and the rear plate,
• wherein each first connection point between the beam and a link rod is formed as a clevis created in the beam,
• wherein a first wall of said clevis is made up of an extension of the front plate, and
• wherein a second wall of said clevis is made up of an extension of the rear plate.