Assembly and method for gauging fuel of electric aircraft

An assembly for gauging fuel of an electric aircraft, comprising:

• a plurality of battery packs of an electric aircraft, wherein each battery pack of the plurality of battery packs comprises a plurality of battery modules;
• at least a battery sensor in communication with the plurality of battery packs, wherein the at least a battery sensor is configured to measure battery data, wherein the battery data comprises a power and a voltage of each of the battery packs of the plurality of battery packs;
• and
• a computing device communicatively connected to the at least a battery sensor, wherein the computing device is configured to:
• receive the battery data from the at least a battery sensor;
• receive flight data, wherein the flight data comprises precipitation data and thrust of one or more flight components of the electric aircraft;
• determine, as a function of the battery data and the flight data, a landing power of the electric aircraft;
• compare the landing power to a landing energy threshold, wherein the landing energy threshold comprises a power-consumption need of the electric aircraft;
• determine a landing recommendation for a landing style of the electric aircraft as a function of the comparison;
• and
• provide the landing power to a user through a display.