What was found
DURING C-CHECK, FOUND AFT WING FILLET PANEL 2208C BETWEEN ATTACH RUB STRIP AND FUSELAGE SKIN IS CORRODED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND AFT WING FILLET PANEL 2208C BETWEEN ATTACH RUB STRIP AND FUSELAGE SKIN IS CORRODED. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-04. (M)