What was found
DURING C-CHECK, INTERNAL FUSELAGE SKIN BETWEEN FRAMES 11-12 STRINGER 20-21L HAS CORROSION. MX REPAIRED SKIN IAW EC5330-02719. 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, INTERNAL FUSELAGE SKIN BETWEEN FRAMES 11-12 STRINGER 20-21L HAS CORROSION. MX REPAIRED SKIN IAW EC5330-02719. ACFT APPROVED FOR RETURN TO SERVICE.