Patent ID: 8336812

Claim:
An engine attachment for an assembly system configured to be mounted between a rigid structure of an attachment strut of an aircraft and an engine, the attachment comprising: a main body; a rudder bar with an articulated mounting on the main body by a first hinge pin; and two thrust absorption rods each with a rear end connected to the rudder bar, wherein the main body includes a first main brace and a second main brace superimposed on the first main brace, wherein the first hinge pin is composed by a first portion of pin and a second portion of pin, wherein the first portion of pin is made in one piece with the first main brace and the second portion of pin is made in one piece with the second main brace, and the first and second main braces jointly define a stop limit surface configured to limit rotation of the rudder bar around the first hinge pin, the first hinge pin extending from a surface of the first and second main braces that is opposite a surface of the first and second main braces that contacts the attachment strut.