Aircraft engine attachment comprising inclined fixing elements, aircraft comprising said engine attachment and method for fixing an engine to an aircraft pylon using said engine attachment

An engine attachment configured to link an engine and an aircraft pylon, the engine attachment comprising:

• a first end fitting having a plate, configured to be pressed against a contact surface of the pylon, and two mutually parallel wings linked to the plate,
• a joining piece, configured to be linked to the engine, positioned between the wings of the first end fitting and linked to the first end fitting by a first link system,
• fixing elements, configured to link the first end fitting and the pylon, including first and second fixing elements positioned between the wings of the first end fitting,
• for each of the fixing elements, through holes provided in the plate of the first end fitting,
• wherein, for each of the first and second fixing elements, the through holes of the plate of the first end fitting have axes of revolution forming an angle of between 10 and 45° with a vertical median plane, in order for the first and second fixing elements to be able to be put in place and removed in the presence of the joining piece linked to the first end fitting by the first link system.