SYSTEMS AND METHODS FOR A CHARGING PORT OF AN ELECTRIC VEHICLE

An electric aircraft charging connector, including a direct current pin and/or an alternating current pin. The connector including a ground pin, the ground pin providing a grounded connection. The connector also including a resistance sensor, the resistance sensor electrically connected to the direct current pin and/or the alternating current pin, and the ground pin, the resistance sensor configured to measure a resistance datum, the resistance datum including: a first resistance, the first resistance comprising a measurement of resistance between the direct current pin and the ground pin; and a second resistance, the second resistance comprising a measurement of resistance between the alternating current pin and the ground pin. The connector also including a controller, the controller configured to: receive the resistance datum from the resistance sensor; and compare the resistance datum to a threshold resistance datum.