As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FORWARD FUSELAGE, FROM FR04+165MM TO FR05+170MM, BETWEEN STRINGER 23RH+45MM AND STRINGER 25RH+95MM, EXTERNAL SKIN WITH EXISTING REPAIR WITHOUT TRACEABILITY OF MATERIALS. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-029872 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2023- 18861-R00 INSTRUCTIONS ( FOR ADDITIONAL DETAILS SEE COOPESA JOB: A1N199 SPECIAL ITEMS : 21-84 ).