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 CRACK UNDER THE EXISTING REINFORCEMENT LOCATED IN THE LH WING UPPER SKIN AT SPAR II OVER RIB 10.WAS REPAIRED FOLLOWING EMB REPAIR INSTRUCTIONS UNDER ETD2023-190-004421 REV / AND COOPESA EO# COO-EO-2023-17209-R00 AND APPROVED ON ANAC F-200 PROVIDED BY EMB.