As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD WING TO BODY FAIRING STRAP CORRODED BETWEEN 5 AND 6 0 CLOCK POSITION. BLENDED CORROSION ON FWD WING TO BODY FAIRING STRAP BETWEEN 5 AND 6 0 CLOCK POSITION PER SRM 51-10-03. NOMINAL MATERIAL THICKNESS OF STRAP IS 0.050". MATERIAL REMOVED 0.003" . MATERIAL REMAINING IS 0.047". FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS (<30%) PER SRM 53-04-02-01-02.