Aircraft propulsion assembly comprising an engine having a reactor core and a fan casing, a primary structure of a pylon, and also an engine attachment having a rear engine attachment, a pair of thrust rods, a first front engine attachment connecting the primary structure and the reactor core, and also a second front engine attachment connecting the primary structure and the fan casing, - the first front engine attachment comprising: o a continuation positioned at the front of the primary structure, having a first end (94.1) connected to the primary structure and a second end (94.2) remote from the primary structure, o at least one shackle, o a first sliding and pivoting connection oriented in a longitudinal direction parallel to an axis of rotation of the engine, having a first pivot axis approximately parallel to the longitudinal direction, connecting the second end (94.2) of the continuation and the shackle and incorporating a ball, o at least one engine connection connecting the shackle and the reactor core of the engine, - the second front engine attachment comprising: ∘ a link rod which extends between a first and a second end (116.1, 116.2), o a second sliding and pivoting connection oriented in the longitudinal direction, having a second pivot axis approximately parallel to the longitudinal direction, connecting the second end (116.2) of the link rod and the fan casing and incorporating a ball, o at least one pivoting connection, having a pivot axis approximately parallel to a horizontal transverse direction, connecting the first end (116.1) of the link rod and the primary structure. - the first front engine attachment comprising: o a continuation positioned at the front of the primary structure, having a first end (94.1) connected to the primary structure and a second end (94.2) remote from the primary structure, o at least one shackle, o a first sliding and pivoting connection oriented in a longitudinal direction parallel to an axis of rotation of the engine, having a first pivot axis approximately parallel to the longitudinal direction, connecting the second end (94.2) of the continuation and the shackle and incorporating a ball, o at least one engine connection connecting the shackle and the reactor core of the engine, o a continuation positioned at the front of the primary structure, having a first end (94.1) connected to the primary structure and a second end (94.2) remote from the primary structure, o at least one shackle, o a first sliding and pivoting connection oriented in a longitudinal direction parallel to an axis of rotation of the engine, having a first pivot axis approximately parallel to the longitudinal direction, connecting the second end (94.2) of the continuation and the shackle and incorporating a ball, o at least one engine connection connecting the shackle and the reactor core of the engine, - the second front engine attachment comprising: ∘ a link rod which extends between a first and a second end (116.1, 116.2), o a second sliding and pivoting connection oriented in the longitudinal direction, having a second pivot axis approximately parallel to the longitudinal direction, connecting the second end (116.2) of the link rod and the fan casing and incorporating a ball, o at least one pivoting connection, having a pivot axis approximately parallel to a horizontal transverse direction, connecting the first end (116.1) of the link rod and the primary structure. ∘ a link rod which extends between a first and a second end (116.1, 116.2), o a second sliding and pivoting connection oriented in the longitudinal direction, having a second pivot axis approximately parallel to the longitudinal direction, connecting the second end (116.2) of the link rod and the fan casing and incorporating a ball, o at least one pivoting connection, having a pivot axis approximately parallel to a horizontal transverse direction, connecting the first end (116.1) of the link rod and the primary structure.