Abstract: A method and device control the thrust of a multi-engine aircraft. At least one engine command is determined by a command determining unit, with the determined command commanding each engine that has not failed to deliver a thrust substantially equal to a reduced thrust value. A command application unit is configured to apply the determined command to each aircraft engine that has not failed. The reduced thrust value is determined, by a weight determining device, according to the current weight of the aircraft and according to a reduced thrust value FOEI, which is calculated by a thrust calculation unit.

Abstract: The device (1) comprises a means (3) for determining the current weight of the aircraft, a means (4) for calculating a reduced thrust value which is proportional to the said current weight, a means (5) for determining at least one engine command, so that the engines deliver a thrust equal to the said reduced thrust value, and a means (7) for applying this command to those engines of the aircraft which have not failed.