As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REF CMM 78-31-37 REV 024 01JUL2012 FIG 19. THE OUTBOARD SURFACE OF THE 315A2311-1 HINGE BEAM (DETAIL PART OF THE 315A2310-1 FITTING ASSY) HAS AN AREA OF MATERIAL WEAR LOCATED 13.0" FWD FROM AFT END OF PART MEASURING 1.20" LONG .21" WIDE. EDDY CURRENT INSPECTION PER NDT MANUAL WAS PERFORMED AROUND THE PERIMETER OF THE MATERIAL WEAR AND THE SURFACE OPPOSITE OF THE MATERIAL WEAR. NO CRACK-LIKE INDICATIONS FOUND. ULTRASONIC THICKNESS REVEALS A .100 NOMINAL THICKNESS OUTSIDE OF MATERIAL WEAR AND .034 MINIMUM REMAINING THICKNESS AT THE BOTTOM OF THE WEAR.