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

A front engine attachment system for 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 that is fastened to the front face and to which a link-rod system is fastened on either side of a median plane,
• wherein the beam is made up of a front plate and a rear plate that are fastened together in a removable manner,
• wherein the rear plate is pressed against the front face and
• wherein the front plate is disposed in front of the rear plate, and
• wherein each link-rod system is fastened only to the rear plate in an articulated manner by at least one first connection point and is intended to be fastened to a front part of the engine in an articulated manner by at least one second connection point,
• wherein each link-rod system comprises a front link rod and a rear link rod,
• wherein each first connection point between the beam and a link-rod system is formed as a clevis, wherein one wall of said clevis is made up of the front rod of said link-rod system, wherein another wall of said clevis is made up of the rear link rod of said link-rod system,
• wherein the rear plate is disposed between the front and rear link rods, and
• wherein a pin passes through a bore in each link rod and a bore in the rear plate.