What was found
FOUR DENTS ON VERTICAL FIN LEADING EDGE PANEL. BLENDED OUT DAMAGE PER BOEING SRM 51-10-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUR DENTS ON VERTICAL FIN LEADING EDGE PANEL. BLENDED OUT DAMAGE PER BOEING SRM 51-10-01.