Systems and methods for data verification at start up

A system comprising:

• a plurality of software systems associated with an electric aircraft;
• a sensor configured to detect an operational datum from an electric component of the electric aircraft;
• a display;
• and
• a processor communicably coupled to the plurality of software systems and the display, at startup of the electric aircraft, the processor configured to:
• identify a software datum of each software system of the plurality of software systems;
• receive the operational datum from the sensor;
• retrieve a historical performance datum of the electric component from a previous flight;
• determine a plurality of software status datum by determining, for each software system of the plurality of software systems, a respective software status datum based on a comparison of the respective software datum to an acceptance criterion and further based on an assessment of the operational datum relative to an operational threshold, wherein the assessment of the operational datum relative to an operational threshold includes a rate of degradation determined based on a comparison of the operational datum to the historical performance datum;
• and
• initiate display of an output datum in a graphical form via the display, the output datum including the plurality of software status datum.