As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING ROOT AREA UPPER SKIN SURFACE CORRODED AT FUSELAGE STA 616 TO 617.5 AT WBL 85.0 TO 87.0. REMOVED CORROSION DAMAGE PER SRM 57-20-01, ROTO PEENED, ALODINED & RESTO RED PAINT PER SRM 51-20-01.THE REPAIR IS APPROVED BY FAA 8100-9 DATED NOV 27TH 2005.