A method for distributing electric power from a power source of an aircraft to a plurality of electrically-powered hydraulic pumps (32A-32N) of the aircraft during a limited power availability condition, the method comprising: distributing electric power from the power source of the aircraft operating during the limited power availability condition to the plurality of electrically-powered hydraulic pumps (32A-32N) of the aircraft; receiving one or more signals indicative of a demand for electric power by one or more of the plurality of electrically-powered hydraulic pumps (32A-32N) of the aircraft; and adjusting the power distribution to the one or more of the plurality of electrically-powered hydraulic pumps (32A-32N) based on the demand for electric power by the one or more of the plurality of electrically-powered hydraulic pumps to maintain an overall power consumption of the one or more of the plurality of electrically-powered hydraulic pumps (32A-32N) at or below a threshold; wherein adjusting the power distribution comprises adjusting a set point of one or more current limiters respectively associated with one or more of the plurality of the electrically-powered hydraulic pumps (32A-32N); wherein the one or more signals indicative of the demand for electric power are indicative of an operating pressure of the one or more of the plurality of electrically-powered hydraulic pumps (32A-32N), and the method further comprising: adjusting the set point associated with a limiter for an electrically-powered hydraulic pump having a lower operating pressure to a higher value than a set point associated with a limiter for an electrically-powered hydraulic pump having a higher operating pressure. distributing electric power from the power source of the aircraft operating during the limited power availability condition to the plurality of electrically-powered hydraulic pumps (32A-32N) of the aircraft; receiving one or more signals indicative of a demand for electric power by one or more of the plurality of electrically-powered hydraulic pumps (32A-32N) of the aircraft; and adjusting the power distribution to the one or more of the plurality of electrically-powered hydraulic pumps (32A-32N) based on the demand for electric power by the one or more of the plurality of electrically-powered hydraulic pumps to maintain an overall power consumption of the one or more of the plurality of electrically-powered hydraulic pumps (32A-32N) at or below a threshold; wherein adjusting the power distribution comprises adjusting a set point of one or more current limiters respectively associated with one or more of the plurality of the electrically-powered hydraulic pumps (32A-32N); wherein the one or more signals indicative of the demand for electric power are indicative of an operating pressure of the one or more of the plurality of electrically-powered hydraulic pumps (32A-32N), and the method further comprising: adjusting the set point associated with a limiter for an electrically-powered hydraulic pump having a lower operating pressure to a higher value than a set point associated with a limiter for an electrically-powered hydraulic pump having a higher operating pressure.