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 FR23, STRINGER 25RH+173MM EXTERNAL SKIN WITH EXISTING TOOL MARK. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2024-190-000066 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2024-19125-R00 ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N232 ITEM: 21-96 ).