A method for detecting the opening of a thrust reverser for a jet engine of an aircraft is disclosed. According to the method, an operating parameter of the turbojet (1) is determined being responsive to the opening of a mobile element (2a, 2b) of the thrust reverser and reacting to such an opening by a sudden variation of the value thereof, the parameter is measured continuously and the mobile element (2a, 2b) is considered as being opened when the sudden variation is detected.
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