As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT OB FLAP HAS THE OB HING BEAM DAMAGED BY A SCREW BETWEEN THE HINGE AND THE FITTING. CLEANED DAMAGED AREA, BLENDED SMOOTH, PERFORMED ROTO/FLAP PEEN OF REPAIR AREA, ALODINED AND TREATED IAW ORIGINAL CONFIGURATION IAW WVAC EO 601R-57-4391.