As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENG PYL OTBD MIDSPAR FTG CLOSEOUT ANGLE INBD BOLT HOLE CRACKED. ACP SMC 017 ACP PER EVA 80724. ON WU E9784H. VERIFIED WITH HFEC CRACK CONTAINED BY STOP DRILL. ACP PER AMT. FASTENERS REMOVED AND OPEN HOLE INSPECTION ACCOMPLISHED. NO CRACKS FOUND.