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 BLEND OUT EXCEEDED 50 PERCENT OF THE SKIN THICKNESS. ALLIANCE INTENDS TO PERFORM A REPAIR FOLLOWING SRM II 53-22-01 REPAIR 63 GUIDELINES; HOWEVER, THE DAMAGED AREA IS LOCATED IN A NON-ALLOWED REPAIR AREA AS PER PARAGRAPH 3.B. AND FIGURE 204. WAS REPAIRED FOLLOWING EMB REPAIR INSTRUCTIONS UNDER ETD2023-190-004867 REV / AND COOPESA EO# COO-EO-2023-17230-R00 AND APPROVED ON ANAC F-200 PROVIDED BY EMB.