As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE STRUCTURAL INSPECTION, IT WAS FOUND AN EXISTING REPAIR WITHOUT RECORDS IN THE FUSELAGE SKIN, LOCATED BETWEEN FRAMES 83-84 AND BETWEEN STRINGERS 13L-16L. WAS REPAIRED FOLOWING EMB REPAIR INSTRUCTIONS UNDER ETD2023-190-003976 REV / AND COOPESA EO# COO-EO-2023-17176-R00 AND APPROVED ON ANAC F-200 PROVIDED BY EMB.