Abstract: A suspension part for mounting a turbojet engine includes two ends equipped with two elements, juxtaposed in a widthwise direction of the suspension part, for fixing the suspension part to the fixed structure. The ends are shaped into pairs of yokes respectively flanking connecting rods and each including fixing elements and a bearing of a journal of a connecting rod which bearing is situated underneath a fixing element. The suspension part also includes slots passing through the two ends of the suspension part and running between the yokes without running over a central portion of the suspension part. Each of the yokes has an upper portion with an additional thickness located on an inside of each of the yokes.

Abstract: The invention concerns a suspension part (1) comprising ends supporting connecting rods (8 and 9) articulated to a turbojet engine (3) which is constructed such that the ends form a pair of yokes (5) separated by a slot (19) bisecting the part (1) over part of its length so as to stop fatigue crack propagation (20). The fixing elements (11) comprising lock bolts (13) are arranged in enlarged portions (15) of the yokes (5) which extend above the connecting rods (8) and (9), thereby ensuring static resistance of the yokes (5) when the counterpart has given way. Said arrangement also reduces cantilever between the fixing elements (11) and the connecting rod (8) and (9).