What was found
DURING C-CHECK, FUSELAGE SKIN CORRODED BETWEEN FRAME 57-58, STR 20R-19R. REPAIRED SKIN IAW EC5330-03001. ACFT WAS 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, FUSELAGE SKIN CORRODED BETWEEN FRAME 57-58, STR 20R-19R. REPAIRED SKIN IAW EC5330-03001. ACFT WAS APPROVED FOR RETURN TO SERVICE.