As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CLT - DURING Q-1 CHECK VISUAL, INSPECTION FOUND A 1 INCH CRACK IN THE UPPER FORWARD AND LOWER AFT CORNERS AT ACCESS PANEL NR 572LL OPENING ON SKIN. TRIMMED OUT DAMAGE AND INSTALLED DOUBLER PER REPAIR DOCUMENT 54-50-04C AND EA 60072. (M)