The invention relates to an assembly between a front fitting and the traction coupling of the two lateral boxes of the horizontal stabilizer of an aircraft comprising a front fitting (1, 1a and 1b), a front shear plate (2), an upper shear plate (4), a lower shear plate (5) and a "rib post" union piece (3) in such a way that the loads being transferred to the lateral boxes are minimized, and at the same time it allows a proper trimming of the horizontal stabilizer. Moreover, the present invention describes a compact front fitting, made of one piece, as a whole, and in composite material.
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