Decompression assembly for use in an aircraft, the decompression assembly comprising: - a cabin lining element, - an opening formed in the cabin lining element, and - an air channel which is arranged adjacent to a rear face of the cabin lining element and connected to the opening formed in the cabin lining element, whe rein the air channel is provided with an air outlet which, during normal operation of the decompression assembly, is adapted to discharge air exiting an aircraft cabin region delimited by the cabin lining element through the opening formed in the cabin lining element into an aircraft area located between the cabin lining element and an aircraft outer skin, a first decompression opening, and a first decompression flap which, during normal operation of the decompression assembly, is adapted to close the first decompression opening provided in the air channel and which, in the event of a rapid decompression, is adapted to open the first decompression opening so as to allow a pressure equalization between the aircraft cabin region delimited by the cabin lining element and the aircraft area located between the cabin lining element and the aircraft outer skin; characterized in that the air channel further comprises: a second decompression opening, and a second decompression flap which, during normal operation of the decompression assembly, is adapted to close the second decompression opening provided in the air channel and which, in the event of a rapid decompression, is adapted to open the second decompression opening so as to allow a pressure equalization between the aircraft cabin region delimited by the cabin lining element and the aircraft area located between the cabin lining element and the aircraft outer skin. - a cabin lining element, - an opening formed in the cabin lining element, and - an air channel which is arranged adjacent to a rear face of the cabin lining element and connected to the opening formed in the cabin lining element, whe rein the air channel is provided with an air outlet which, during normal operation of the decompression assembly, is adapted to discharge air exiting an aircraft cabin region delimited by the cabin lining element through the opening formed in the cabin lining element into an aircraft area located between the cabin lining element and an aircraft outer skin, a first decompression opening, and a first decompression flap which, during normal operation of the decompression assembly, is adapted to close the first decompression opening provided in the air channel and which, in the event of a rapid decompression, is adapted to open the first decompression opening so as to allow a pressure equalization between the aircraft cabin region delimited by the cabin lining element and the aircraft area located between the cabin lining element and the aircraft outer skin; characterized in that the air channel further comprises: a second decompression opening, and a second decompression flap which, during normal operation of the decompression assembly, is adapted to close the second decompression opening provided in the air channel and which, in the event of a rapid decompression, is adapted to open the second decompression opening so as to allow a pressure equalization between the aircraft cabin region delimited by the cabin lining element and the aircraft area located between the cabin lining element and the aircraft outer skin. an air outlet which, during normal operation of the decompression assembly, is adapted to discharge air exiting an aircraft cabin region delimited by the cabin lining element through the opening formed in the cabin lining element into an aircraft area located between the cabin lining element and an aircraft outer skin, a first decompression opening, and a first decompression flap which, during normal operation of the decompression assembly, is adapted to close the first decompression opening provided in the air channel and which, in the event of a rapid decompression, is adapted to open the first decompression opening so as to allow a pressure equalization between the aircraft cabin region delimited by the cabin lining element and the aircraft area located between the cabin lining element and the aircraft outer skin; characterized in that the air channel further comprises: a second decompression opening, and a second decompression flap which, during normal operation of the decompression assembly, is adapted to close the second decompression opening provided in the air channel and which, in the event of a rapid decompression, is adapted to open the second decompression opening so as to allow a pressure equalization between the aircraft cabin region delimited by the cabin lining element and the aircraft area located between the cabin lining element and the aircraft outer skin. a second decompression opening, and a second decompression flap which, during normal operation of the decompression assembly, is adapted to close the second decompression opening provided in the air channel and which, in the event of a rapid decompression, is adapted to open the second decompression opening so as to allow a pressure equalization between the aircraft cabin region delimited by the cabin lining element and the aircraft area located between the cabin lining element and the aircraft outer skin.