Mounting device for an aircraft engine comprising two thrust recovery rods with a double rear mechanical connection

A mounting device for an aircraft engine mounted on a rigid structure, said mounting device comprising:

• a thrust load recovery device for recovering the thrust loads generated by the engine, said thrust load recovery device comprising a crossbar and two lateral thrust load recovery rods each having a rear end mounted on the crossbar via, a first mechanical connection, and
• at the rear end of each of the two lateral thrust load recovery rods, a second mechanical connection with play between said rear end and a support fitting integral with the rigid structure,
• wherein said first mechanical connection comprises two pins, each pin being provided on an end of the crossbar and passing through an orifice provided in a corresponding rear end of one of the lateral thrust load recovery rods, each of the two pins of the cross bar being provided on the crossbar so as to extend substantially transversely relative to said mounting device.