METHOD AND SYSTEM FOR A TWO-MOTOR PROPULSION SYSTEM FOR AN ELECTRIC AIRCRAFT

Aspects relate to an electric aircraft having a two-motor propulsion system and methods for use. An exemplary electric aircraft includes a flight component attached to the electric aircraft, where the flight component is configured to generate thrust, a first electric motor and a second electric motor, where each of the first electric motor and the second electric motor are mechanically connected to the flight component and configured to provide motive power to the flight component, and the second electric motor is able to provide motive power to the flight component if the first electric motor is inoperative.