FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft tail. Aircraft tail comprises engine attachment structure 14 extending through fuselage first and second openings 18, 18'. Said structure comprises means to attach it to fuselage 6 and including first fasteners connecting the structure to first frame 50 making the first opening 18 and second fasteners to connect it to frame 50 to make second opening 18'. In compliance with this invention, said fasteners comprise additional at least one link 66 to take up forces with its first end secured at structure 14 and opposite end secured to fuselage between said first and second openings 18, 18'.
EFFECT: decreased weight.
21 cl, 15 dwg
