As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING STRUCTURAL INSPECTION, AN EXISTING REPAIR WAS FOUND ON THE FUSELAGE SKIN AT FR19 BETWEEN STR-27R. ACCORDING TO PREVIOUS OPERATOR DOCUMENTATION, THE REPAIR WAS PERFORMED UNDER ETD2025-190-000892 GUIDELINES. DUE TO ITS CONDITION (TOOL MARKS AND POORLY DRIVEN RIVET HEADS) THE REPAIR DOUBLER WAS REMOVED FOR REPLACEMENT. THIS CONDITION WAS REPORTED AND REPAIRED IAW ETD2025-190-927001 DTD AUG 22 2025 AND DOCUMENTED COOPESA COO-EO-2025-22844-R00 , UNDER JOB A1Q176 NRI 21-32