As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT PYLON IB AFT FRAME TOP SURFACE AT PANEL 5735L NICKED AND GOUGED BEYOND LIMITS AT IB FASTENER HOLE; FABED SHIM AND FLAP PEENED DAMAGED AREA AND SHIM IAW ENG SUPPORT/REPAIR SOPM 20-10-03 ER 0357540033-DL1; HFEC INSPECTED AREA NO CRACKS NOTED PER NDT; TREAT AND PRIME IAW 51-20-01; INSTALLED IAW 51-40-02