| 摘要 |
Aircraft with ventral fairing and seal for such an aircraft. According to the invention, in the slots (11) between said ventral fairing (6) on the one hand, and the fuselage or flying surface (5), on the other hand, is disposed a seal (16, 2) provided with an end lip (17) and with a radially elastic bead (19), which are able to be applied with leaktightness against said fuselage or said flying surface, respectively.
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