As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FORWARD FUSELAGE, BETWEEN FR16+250MM AND FR18+80MM, AND BETWEEN STRINGER 20RH AND STRINGER 21RH, EXISTING SKIN REPAIR EVALUATION. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030699 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023-18944-R01 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEM 21-22 ).