FIELD: aircraft.
SUBSTANCE: invention relates to devices for ground handling of aircraft. The device for mounting and dismantling the rotating leading edge of an aircraft contains a common platform (6), installed with the possibility of tilting, on which right and left saddles (7) are removably installed at the edges, interconnected by a welded tie (9) and connected by side screws (10) on each side. Between the saddles (7) in the middle part of the common platform (6) there is a roller and a system of middle levers, including upper and lower middle levers designed to rotate the jib. Each saddle is U-shaped with a larger and smaller supports, between which a groove is placed. Each saddle is connected to a common platform using a lever system consisting of an upper lever and a lower lever.
EFFECT: increased accuracy of installation of the aircraft leading edge on the aircraft wing.
6 cl, 20 dwg
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