What was found
NON ROUTINE CHECK, CORROSION FOUND ON FWD AND AFT BORES ON OTBD ATTACH FITTING, ALSO FWD BORE INBD FITTING OF SLAT PANEL NR 3LT. REPAIRED IAW SRM 57-02, PAR 9, TABLE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NON ROUTINE CHECK, CORROSION FOUND ON FWD AND AFT BORES ON OTBD ATTACH FITTING, ALSO FWD BORE INBD FITTING OF SLAT PANEL NR 3LT. REPAIRED IAW SRM 57-02, PAR 9, TABLE 1.