The invention relates to a method of extracting at least one foreign body nestled within a blade (110) of a high pressure distributor (100) of a turbojet, said high pressure distributor comprising blades (110). hollow and fixed between two annular shrouds forming a gas circulation stream, each blade being coated with a thermal barrier and pierced with at least one cavity at least partially blocked by a first closure plate (140), brazed, comprising the following operations: - cutting (310) of the first closure plate, - extraction (320) of the foreign body from the cavity, - endoscopic inspection (330) of a space inside the cavity so as to verify that no body foreign remains, - positioning (340) of a second closure plate on the cavity, and - brazing (350) of the second closure plate directly on the distributor with the blades coated with the thermal barrier.
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