Patent ID: 8944382
Filing Date: 2015-02-03
Classification: B64C,B64F,Y10T

Abstract:
1. A method for mounting an aircraft component on an aircraft, wherein in a mounted state the aircraft component is movable between a first operating position and a second operating position and wherein in the second operating position the aircraft component is mounted on the aircraft and extended from a mounting area of the aircraft and in the first operating position the aircraft component is mounted on the aircraft and taken up and received within the mounting area, wherein the method comprises: measuring the mounting area, in order to obtain data characteristic of at least one of the shape and the dimensions of the mounting area; projecting the data characteristic of the at least one of the shape and the dimensions of the mounting area onto the aircraft component arranged in the second operating position; and adjusting the aircraft component when arranged in the second operating position with reference to the projection of the data characteristic of the at least one of the shape and the dimensions of the mounting area.