What was found
CORROSION ON LOWER LEADING EDGE SKIN 39.0 INCHES FROM INBOARD END NUMBER 1 SLAT. CORROSION REMOVED AND HFEC DETERMINED NO CRACKS ON REMAINING .052. INSTALLED REPAIR FILLER DOUBLER SHIM PER SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON LOWER LEADING EDGE SKIN 39.0 INCHES FROM INBOARD END NUMBER 1 SLAT. CORROSION REMOVED AND HFEC DETERMINED NO CRACKS ON REMAINING .052. INSTALLED REPAIR FILLER DOUBLER SHIM PER SRM 51-40-02.