A method for designing repair kits for a predefined area of the external/internal structure of an aircraft, the repair kits each including an external/internal structural part having predefined shape and size, suitable for being placed within the existing external/internal structure, instead of an equivalent shape including a damaged area, which can be removed or not, the method including creating a range of standardised repair kits, optimized according to an estimate of the most likely types of accidental damage in the studied area.
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