FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to fuselage tail with module tail cowling. Aircraft tail includes tail cowling jointed to the other fuselage tail section by appropriate connection system. The latter comprises three brackets located at angles of triangle, compensator and extra standby coupling link. First and second brackets are levelled either from above or from below, each on one side of fuselage tail. Note here that said compensator is arranged between said first and second brackets. Extra standby coupling link is mounted opposite said compensator, under third bracket provided it is located above and above third compensator if it is located below.
EFFECT: ease of assembly and replacement of cowling.
6 cl, 7 dwg
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