| CPC G05D 1/102 (2013.01) [B64D 27/30 (2024.01); G08G 5/50 (2025.01); G08G 5/55 (2025.01)] | 20 Claims |

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1. An apparatus for guiding a transition between flight modes of an electric aircraft, wherein the apparatus comprises:
at least a sensor configured to detect a movement datum of an electric aircraft;
a flight controller communicatively connected to the at least sensor, wherein the flight controller is configured to:
receive the movement datum from the at least a sensor;
determine a current flight mode of the electric aircraft as a function of the movement datum;
generate a guidance datum as a function of a change in flight mode and the movement datum, wherein the generation of the guidance datum comprises an aircraft speed determination;
communicate the movement datum and the guidance datum to a pilot indicator in communication with the flight controller; and
display the movement datum and the guidance datum using the pilot indicator.
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