As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER CENTER FUSELAGE I, AT FR28+380MM STRINGER 27R+91MM, SKIN PANEL WITH LIGTHNING STRIKE. NOTE: THE FUELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2024-190-000510 GUIDELINES AS STATED IN COPESA ENGINEERING ORDER NO: COO-EO-2024-19143-R00 ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N232 ITEM 21-142 ).