Patent ID: 11941925
Assignee: BETA AIR LLC
Field: Computer technology (Electrical engineering)
Classification: CPC G  B | IPC B  G

Claim 10:
11. A method of use for a monitoring system for an electric aircraft, wherein the method comprises:
generating, using at least a senor, a failure datum wherein the failure datum includes a datum regarding a condition of an electric motor;
generating, using a crew alerting system (CAS), a checklist comprising a plurality of branches, each branch comprising a plurality of remedy data configured to address the failure datum for the electric motor;
determining, using the CAS, a first branch of the plurality of branches a function of the failure datum;
displaying, using the CAS, the plurality of remedy data for the first branch using a pilot display, wherein the plurality of remedy data is displayed with increasing intrusiveness from a least intrusive remedy that is expected to be the least intrusive to a flight plan or operation of the aircraft to a most intrusive remedy that is expected to be the most intrusive to a flight plan or operation of the aircraft;
prompting, using the CAS, a pilot to apply a remedy datum of the plurality of remedy data for the first branch using the pilot display as a function of the plurality of remedy data, wherein correlations between the failure datum and the remedy datum are generated from past failure data and past remedy data;
applying, using the CAS, the remedy datum; and
providing, using the CAS, an indication of the condition of the electric motor using the pilot display as a function of the application of the plurality of remedy data.