Electric charging station for an electric vehicle and a method for its use

An electric charging station for an electric aircraft, wherein the electric charging station comprises:

• a charging connector, wherein the charging connector is configured to couple with an electric vehicle port of an electric aircraft for charging a battery of the electric aircraft;
• a charging cable electrically connected to the charging connector, wherein the charging cable is configured to carry electricity;
• an energy source, wherein the energy source is electrically connected to the charging cable;
• a first fluidic connector, wherein the first fluidic connector is configured to couple with at least the electric vehicle port;
• a battery temperature regulating element thermally connected to at least the battery of the electric aircraft through at least the electric aircraft vehicle port and comprising at least a coolant flow path;
• a coolant temperature sensor, wherein the coolant temperature sensor is configured to generate a coolant temperature datum as a function of a coolant temperature;
• and
• a computing device communicatively connected to the battery temperature regulating element and the coolant temperature sensor, wherein the computing device is configured to:
• receive the coolant temperature datum from the coolant temperature sensor;
• regulate the coolant temperature;
• and
• modify a battery temperature of the battery of the electric aircraft using the battery temperature regulating element as a function of coolant flow.