As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE IN HEAVY MX PERFORMING INSPECTIONS CORROSION WAS NOTED AT THE LT WING, LOWER SKIN FWD OF FRONT SPAR WS 250-287 BEHIND THE NR1 & NR2 KRUGER FLAP. CORROSION FOUND TO BE OUT OF LIMITS. PERFORMED BLEND-OUT IAW RES-W1 NR 2002564-12 LOSS OF MATERIAL IS .095". NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.