Method and device for controlling the thrust of a multi-engine aircraft

A means (3) by which a device (1) determines the present weight of an airplane, and a means (4) to calculate a reduction thrust value proportional to this present weight, It opts for at least one engine instructions, and an engine consists of a means (5) to transmit a thrust equal to the above-mentioned reduction thrust value, and a means (7) to give the above-mentioned instructions to an engine with which an airplane is not out of order. [Chosen drawing] Drawing 1