As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING INBOARD FLAP OUTBOARD HINGE LOCATION NR 1 INBOARD AND OUTBOARD LUG HAS CORROSION. REMOVED CORROSION IAW DACCMM 57-44-07. FOUND TO BE STRUCTURALLY ACCEPTABLE IAW EA8-8750-81474. ALODINED AND PRIMED LUG FACES IAW DC10 SRM 51-21-01 VOLUME II. BEGINNING SURFACE 1.255 INCH INBOARD FINAL 1.2400 INCH OUTBOARD 1.2360 INCH. MATERIAL REMOVED INBOARD .015 INCH OUTBOARD .019 INCH FOUND OUT OF LIMITS IAW DACCMM 57-44-07.