Patent ID: 7909302

Claim:
An aircraft engine attachment configured to be positioned between an engine and a mount for the engine, the attachment comprising: a first securing device configured to be secured to the engine mount and including two branches, four anchor orifices of one branch facing four anchor orifices of an other branch; and two shackles each including three orifices, two of the orifices of each shackle connected by link pins to the first securing device via respective anchor orifices at a position in between the two branches, and the third orifice of the shackle configured to be secured at an engine clevis, wherein each of the shackles is a structure including two parts of identical shape and identical thickness lying directly adjacent to and contacting one another in a direction orthogonal to a line connecting the four orifices of the one branch, and wherein upon rupture of one of the two parts of identical shape, an other of the two parts of identical shape lying directly adjacent to and contacting the one of the two parts assumes a full load of the shackle.