Patent ID: 8177166

Claim:
A combination of a tail structure and a fuselage section, the tail structure adjoining the fuselage section, the tail structure comprising: A support construction supporting two engines; and A bulkhead unit in a sealing the fuselage section in a pressure tight manner, the bulkhead unit being connected both to the support construction and to the fuselage section so as to form a force flow path between a respective engine and the fuselage section; Wherein the support construction comprises two pylons which are connected to the respective engine and support the respective engine, and Wherein the pylons are formed by a parallelepiped-defining support bar construction with at least one support bar extending diagonally in the parallelepiped, wherein the support construction has a pyramid-shaped base structure made of four support bars for supporting a stabilizing unit, wherein the pylons are fastened to the pyramid-shaped base structure, wherein the support construction has two oblique struts.