FIELD: transport.
SUBSTANCE: aircraft tail comprises tail cowling (1) attached to the fuselage tail structure (2) by the fastening system composed of two top brackets (3), to bottom brackets (4) and split compensator (5). The latter (5) can be adjusted and fixed in axes Z and Y of the Cartesian rectangular coordinates to make the joint move in axis X of said system and guide the tail cowling (1) relative to the other members (2) of said tail section. Assembly of the tail section comprises the steps that follow. Compensator (5), top (3) and bottom (4) brackets are fitted in place. Compensator (5) acts as the guide of the tail cowling for its connection with the other fuselage tail section structure (2). At assembly of said top and bottom brackets (3, 4), said compensator is mounted. Claimed aircraft incorporate the aforesaid fuselage tail section.
EFFECT: perfected design.
8 cl, 12 dwg
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