As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE AT FR18+105MM, STRINGER 26RH+170MM EXTERNAL SKIN WITH LIGHTNING STRIKE. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2024-190-000450 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2024-19140-R00 ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N232 ITEM: 21-86 ).