As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LHW O/B FLAP I/B HINGE (WING SIDE), SIDE LINK ATTACHMENT SPOT FACE FOUND CORRODED. LT FWD O/B FLAP I/B HINGE BARREL NUT HOLE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 PG. 612-615 AND FOUND WITHIN DAC DWG ARC 0502 LIMIT. ORIGINAL THK I/B 0.445" O/B 0.440", REMAINING THK I/B 0.442" O/B 0.437", MATERIAL REMOVED I/B 0.003" O/B 0.003". REPAIR CARRIED OUT AS PER CMM 57-44-08 AND CLASSIFIED MINOR AS PER GMM 6-2-100.