As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE STRUCTURE INSPECTION, WAS FOUND THE RH WING LEADING EDGE BETWEEN RIBS 19 AND 20 THE SKIN WITH CRACK. THE CRACKED AREA WAS TRIMMED OUT FOLLOWING SRM 57-49-01 REP 51 GUIDELINES, HOWEVER, THE FINAL MEASURE AFTER REWORK EXCEEDS THE MINIMUM ALLOWED. THISCONDITION WAS REPORTED TO EMB ASKING FOR REPAIR INSTRUCTIONS. THE CRACKED AREA WASREPAIRED BY ETD2025-190-922570 AND DOCUMENTED BY COOPESA EO COO-EO-2025-22516-R00 DTD JUN 12 2025.