As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L2 DOOR LOWER AFT CORNER FITTING HAS CORROSION AT LOWER FLANGE OF FRAME 68. REMOVED CORROSION & FOUND MATERIAL LOSS TO BE .018 INCHES. ORIGINAL THICKNESS WAS .070 INCHES, BEYOND LIMITS IAW SRM 51-73-11 PARA D 1. R & R L2 DOOR LOWER AFT CORNER FITTING IAW SRM 51-72-11 PARA 1 - 6.