As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK INSPECTION FOUND CORROSION ON THE FUSELAGE SKIN PANELS IN AREA OF THE WING TO BODY FAIRINGS AT LT STA 1531 TO 1821 BETWEEN L-35L AND L-46L AND RT STA 1531 TO 1700 BETWEEN L-43R AND L-46R. REMOVED LWR AFT RUB STRIPS FROM A/C AT AFT WING TO BODY FAIRING AND CORROSION WAS REMOVED AS PER ECRA 242NW-53-DC10-011.