What was found
INSPECTION FOUND THE NR 5 LEADING EDGE SLAT CRACKED AT THREE RIVETS UNDER INBOARD AUXILIARY TRACK. THE CRACKS WERE .25 INCH LONG. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW ECRA 5750-01159.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND THE NR 5 LEADING EDGE SLAT CRACKED AT THREE RIVETS UNDER INBOARD AUXILIARY TRACK. THE CRACKS WERE .25 INCH LONG. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW ECRA 5750-01159.