Method for managing the exiting of a specific-consumption mode of an aircraft turbine engine

Method for managing the exiting of a specific-consumption mode of an aircraft equipped with a first turbine engine operating in a nominal mode and a second turbine engine operating in a standby mode or in a consumption mode intermediate to the standby mode and to the nominal mode of the second turbine engine, the method comprising a step of identifying a need to reactivate the second turbine engine in the nominal mode of said second turbine engine and a step of:

• normal reactivation for a first duration of the second turbine engine in the nominal mode of said second turbine engine when the aircraft and/or the first turbine engine meets a first condition;
• accelerated reactivation for a second duration of the second turbine engine in the nominal mode of said second turbine engine when the aircraft and/or the first turbine engine meets a second condition;
• and
• rapid reactivation for a third duration of the second turbine engine in the nominal mode of said second turbine engine when the aircraft and/or the first turbine engine meets a third condition,
• normal reactivation being preferred over accelerated reactivation, accelerated reactivation also being preferred over rapid reactivation, the first duration being longer than the second duration, and the second duration being longer than the third duration.