Patent ID: 8366040

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 fastening means further comprises at least one effort recovery connecting rod whereof a first end is mounted on the support structure, and the opposite end of which is mounted on the fuselage, spaced away from the first and second openings.