FIELD: aircraft engineering.
SUBSTANCE: invention relates to aviation equipment, particularly, to structural element positioning setting device (1), for example, horizontal tail. Setting device (1) contains at least two loading paths (2, 3), wherein loading paths (2, 3) are formed by group of load transmitting parts. At that, second loading path (3) comprises gap (50, 51) to take elongation of, at least, one part of first loading path (2). Besides, setting device (1) comprises fixing unit (4) with fixation device (40). Fixing device (40) enters gap (50, 51), if first loading path (2) part is damaged.
EFFECT: higher reliability.
10 cl, 9 dwg
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