As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C RT WING LE NR 18 VC FLAP IB ARM OB RIB AT ILES 802 CRACKED. STOP DRILLED CRACK TRIMMED OFF STIFFENER THE REPAIR FTG AND THE REPAIR STRAP INSTALLED IAW HXRS NR R57-41-35055 AND EO B747-5740-19118-A ISSUED FOR REPLACE THE RIB WITHIN 18 MONTHS AND PERFORM REPEAT DETAIL VISUAL INSP. AT 77 DAY INTERVALS FOR GENERAL REPAIR INTEGRITY AND CRACK PROPAGATION.