What was found
INSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 1741 TO 1961, STRINGER 4OR TO 46R. THE SKIN PANEL WAS REPLACED AND REPAIR WAS ACCOMPLISHED IAW SRM 51-10-01, PAGE 18 AND ECRA 5330-02508.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 1741 TO 1961, STRINGER 4OR TO 46R. THE SKIN PANEL WAS REPLACED AND REPAIR WAS ACCOMPLISHED IAW SRM 51-10-01, PAGE 18 AND ECRA 5330-02508.