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 A CRACK UNDER THE EXISTING REINFORCEMENT LOCATED IN THE RH WING UPPER SKIN AT SPAR II OVER RIB 10. WAS REPAIRED FOLLOWING EMB REPAIR INSTRUCTIONS UNDER ETD2023-190-004420 REV A AND COOPESA EO# COO-EO-2023-17310-R00 AND APPROVED ON ANAC F-200 PROVIDED BY EMB.