System and a method for a battery power management system for an electric aircraft

A system for a battery power management system for an electric aircraft, wherein the system comprises:

• at least a flight component of an electric aircraft;
• at least a battery, wherein the at least a battery is configured to power the at least a flight component of the electric aircraft;
• at least a sensor communicatively connected to the at least a battery;
• and
• a controller communicatively connected to the at least a sensor, wherein the controller is configured to:
• receive sensor data from the at least a sensor;
• identify a battery status as a function of the sensor data and a battery threshold;
• and
• control the power from the at least a battery to the at least a flight component of the electric aircraft as a function of the battery status, wherein controlling the power from the at least a battery to the at least a flight component comprises reducing a torque to the at least a flight component.