As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE I, AT FR25+74MM STRINGER 27LH +78MM SKIN PANEL WITH LIGHTNING STRIKE. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2024-190-000632 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2024-19158-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N232 ITEMS: 21-139 & 21-145 ).