As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CENTER FUSELAGE I, LEFT LATERAL SKIN PANEL BETWEEN FR23 AND FR24 AND BETWEEN STRINGER 13LH AND STRINGER 14LH EXISTING REPAIR WITH NOT ACCEPTABLE DOUBLER CORNER GEOMETRY. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2024-190-000372 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2024-19133-R00 ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N232 ITEM 21-146 ).