METHODS AND SYSTEMS FOR MITIGATING CHARGING FAILURE FOR AN ELECTRIC AIRCRAFT

A charging system for mitigating charging failure for an electric aircraft, the system comprising a charger port located on the electric aircraft and configured to mate with a charging connector, a sensor communicatively connected to the charger port and configured to detect a charging datum, and a controller communicatively connected to the charger port and the sensor. The controller is configured to receive charging datum from the sensor, detect a charging failure as a function of a comparison between the charging datum to a pre-set charging datum threshold, and record the charging failure in a database.