The invention discloses a dynamic and static wing involution inspection device and method for an
airplane empennage. Comprising a positioning mechanism (1), the positioning mechanism (1) comprises a sliding rail (3), a
pulley main frame (4) is connected to the sliding rail (3) in a sliding mode, and a folding mechanism (2) is arranged at the end of the sliding rail (3); the
pulley main frame (4) is provided with a static wing V-shaped groove zero point positioner (6) used for supporting and positioning an
airplane empennage static wing. A movable wing turnover mechanism is further arranged on the
pulley main frame (4), the movable wing turnover mechanism comprises a movable wing turnover frame (12) rotationally connected to the pulley main frame (4), and a movable wing V-shaped groove zero-point positioner (7) used for supporting and positioning an
airplane empennage movable wing is arranged on the movable wing turnover frame (12); a driving mechanism A (5) is further arranged on the pulley main frame (4), and the movable wing overturning frame (12) can overturn under the driving of the driving mechanism A (5); the folding mechanism (2) comprises a
fixed frame (10) arranged at the end part of the sliding rail (3), the
fixed frame (10) is rotationally connected with a static wing turning plate (9), and the
fixed frame (10) is also provided with a driving mechanism B (11); and the static wing turning plate (9) can turn over under the driving of a driving mechanism B (11). According to the invention, the folding and checking efficiency and quality of the movable and static wings of the airplane are improved, and the folding consistency and stability of products are greatly improved.