Fuselage skin panel prehension and localized maintenance method for aircraft, involves blocking vent holes with respect to support plate in its prehension position without local deformation of convex side of fuselage skin panel

摘要

The method involves plating a convex side (1a) of a fuselage skin panel (p) of an aircraft against fixed stops (2) with three points, without deformation. A number of vent holes movable with respect to a support plate (1) is applied on the convex side, in the support zone. Each vent hole is blocked with respect to the support plate in its prehension position without local deformation of the convex side. An independent claim is also included for a device to implement a method for prehension and localized maintenance of a fuselage skin panel of an aircraft in an isostatic position.