Patent ID: 8448897

Claim:
A rear part of an aircraft comprising: a fuselage delimiting an inner area of the aircraft; at least two engines; a support structure for the engines, passing through the fuselage at first and second openings formed therein and distributed on either side of a vertical middle plane of the aircraft, the support structure having first and second opposite ends; each of the first and second opposite ends of the support structure protruding outwardly from the fuselage, on either side of the vertical middle plane, respectively, and supporting one of the engines; and fastening means connecting the support structure to the fuselage, comprising first fastening means connecting the support structure to a first casing forming the first fuselage opening and second fastening means connecting the support structure to a second casing forming the second fuselage opening; wherein the first fastening means comprises at least one blocking element of the support structure, under compression loading while bearing on the first casing, and on the support structure, and wherein the second fastening means comprises at least one blocking element of the support structure, under compression loading while bearing on the second casing, and on the support structure.