As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION - NR 4 FLAP TRACK FORWARD END CLEVIS BUSHING HOLE AND OUTSIDE SURFACE CORROSION. BLEND OUT THE CORROSION. SPOT FACE THE FWD END CLEVIS. OVERSIZE THE BUSHING HOLE. NDT MEASURE NO DAMAGE WAS FOUND. FLAP PEEN EACH CLEVIS LUG. FABRICATE AT INSTALL BUSHINGS.