As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SPOT OF LIGHT CORROSION ON UNDER SIDE OF LEFT WING FLAP L/E AT INTERSECTION OF CENTER AND I/B FIXED VANES. MECHANICALLY REMOVED CORROSION .030 MATERIAL LOSS, OUT OF LIMITS. FABRICATED REPAIR DOUBLER FROM .071 7075 T-6 MEASURING 3 X 4.75 AND INSTALLED IAW SRM 578-01 FIG 3, 51-20-0 AND 51-30-1.