Systems and methods for restricting power to a load to prevent engaging circuit protection device for an aircraft

A system for restricting power to a load to prevent engaging a circuit protection device for an electric aircraft, the system comprising:

• at least an energy source of an electric aircraft, wherein the at least an energy source is communicatively coupled to a load of a plurality of loads, wherein the load comprises at least a portion of a propulsion system of the electric aircraft;
• a plurality of sensors mounted on the electric aircraft, wherein each sensor of the plurality of sensors are designed and configured to:
• sense at least an electrical parameter of the at least a portion of the propulsion system of the electric aircraft;
• an aircraft controller communicatively connected to the at least an energy source, wherein the aircraft controller is designed and configured to:
• receive at least an electrical parameter of the at least a portion of the propulsion system of the electric aircraft from the plurality of sensors;
• compare the at least an electrical parameter to at least a current allocation threshold, wherein the current allocation threshold is generated as a function of at least a circuit protection threshold of load;
• detect that the at least an electrical parameter has reached the current allocation threshold;
• calculate a power reduction to the load;
• and
• reduce power from the at least an energy source to each load of the plurality of loads by the power reduction.
• at least an electrical circuit of the electric aircraft, wherein the at least an electrical circuit comprises:
• a circuit protection device communicatively connected to the aircraft controller.