Abstract: An assisted piloting method for an aircraft having at least two engines (2, 3) includes monitoring a set of parameters (Ng, T4, Tq) of the engines. A first limit indicator (10) displays information relating to a value of a limiting parameter of the engines. The limiting parameter is the parameter (Ng, T4, Tq) of the engines that is the closest to its limit. An assisted piloting mode is activated during which each parameter (Ng, T4, Tq) is maintained below a predetermined threshold whenever the first limit indicator is not in a position to display the information.

Abstract: An assisted piloting method for an aircraft having at least two engines (2, 3) for use in the event of a first limit indicator (10) breakdown down, a plurality of monitoring parameters (Ng, T4, Tq) of the engines (2, 3) of said aircraft being monitored, said first limit indicator (10) displaying information relating to a value of a limiting parameter of said engines (2, 3), the limiting parameter being that one of the monitoring parameter (Ng, T4, Tq) of the engines that is the closest to its limits. Under such circumstances, an assisted piloting mode is activated during which each monitoring parameter (Ng, T4, Tq) is maintained below a predetermined threshold whenever said first limit indicator (10) is not in a position to display said information.