In an assembly including a bypass turbine engine and an attachment system attaching the
turbine engine to an aircraft structure, the attachment system includes a mast, at least two
rear attachments connecting the mast to two rear attachment points of the turbine engine,
and a rear covering covering the rear attachments and providing a streamlined fairing. The
rear covering includes two side walls, each including a first portion extending along and in
proximity of the mast and extending rearwards, and a second portion projecting side ways …