What was found
DURING C-CHECK, A CRACK WAS FOUND IN UPPER END OF UPPER ACCESS PANEL FLANGE ON LT WING RIB 1 INSIDE WHEELWELL AFT OTBD CORNER. R & R ACCESS PANEL FLANGE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, A CRACK WAS FOUND IN UPPER END OF UPPER ACCESS PANEL FLANGE ON LT WING RIB 1 INSIDE WHEELWELL AFT OTBD CORNER. R & R ACCESS PANEL FLANGE IAW SRM 51-40-02. ACFT APPROVED FOR RETURN TO SERVICE.