What was found
NR 11 SLAT HAS CORROSION ON STIFFENER INSIDE 625CB COVE PANEL. REMOVED AND REPLACED CORD SPLICE P/N 114T4122-55. INSTALLED WITH HI-LOCKS IAW B767 SRM 51-40-02 PARA 7. ACFT WAS GROUNDED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 11 SLAT HAS CORROSION ON STIFFENER INSIDE 625CB COVE PANEL. REMOVED AND REPLACED CORD SPLICE P/N 114T4122-55. INSTALLED WITH HI-LOCKS IAW B767 SRM 51-40-02 PARA 7. ACFT WAS GROUNDED.