Abstract: A device for suspending a casing of a turbine engine to the structure of an aircraft is provided. The device includes a suspension ring including a plurality of attachment surfaces positioned so as to protrude on the circumference of the suspension ring and having attachment holes for attachment to the structure; a circumferential flange including a plurality of holes for attaching the suspension ring to the casing; and one or several hanging surfaces for hanging at least one piece of equipment, positioned so as to protrude on the circumference of the suspension ring, and having holes for hanging the piece of equipment to the ring.

Abstract: The invention relates to a device (1) for suspending a casing (2) of a turbine engine (3) to the structure (12) of an aircraft, characterized in that it comprises a suspension ring (4), said suspension ring (4) comprising; a plurality of attachment surfaces (33) positioned so as to protrude on the circumference of the suspension ring (4) and having attachment holes (6), for attachment to the structure (12), a circumferential flange (5) comprising a plurality of holes (35) for attaching the suspension ring (4) to the casing (2); one or several hanging surfaces (10) for hanging at least one piece of equipment (15) , positioned so as to protrude on the circumference of the suspension ring (4), and having holes (8) for hanging the piece of equipment (15) to the ring (4). The invention also relates to a turbine engine and to a propulsion assembly comprising such a device.