As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE STRUCTURE INSPECTION, A CRACK WAS FOUND IN THE LH WING LEADING EDGE SKIN BETWEEN RIBS 19 AND 20. THE CRACKED AREA HAS NOT BEEN TRIMMED, HOWEVER, THE FINAL MEASURE AFTER TRIM OUT WILL EXCEED THE MINIMUM ALLOWED IN E190- SRM 57-49-01 REPAIR 51. WAS REPAIRED FOLLOWING EMB REPAIR INSTRUCTIONS UNDER ETD2023-190-004414 REV / AND COOPESA EO# COO-EO-2023-17195-R00 AND APPROVED ON ANAC F-200 PROVIDED BY EMB.