FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Connector (41, 71) for fastening of aircraft vertical tail unit is made of composite material and includes first part (43, 73) including lugs (45, 45'; 75, 75') fastening of said unit and vertical walls (47, 47'; 77, 77') for attachment of connector (41, 71) to frames (7). Two extra parts (49, 49'; 79, 79') including horizontal walls (51, 51'; 81, 81') serve for attachment of connector (41, 71) to skin (5). Connector (71) for attachment with inclined load comprises also the second pair of angular parts (90, 90') with vertical walls (93, 93') for attachment with lugs (75, 75'). Versions of proposed method describe the assembly of connectors (42, 71).
EFFECT: better distribution of loads.
6 cl, 7 dwg
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