What was found
INSPECTION FOUND A .50 INCH CRACK IN LOWER SKIN OF NR 5 SLAT. THE CRACK WAS LOCATED AT CORNER OF SKIN BELOW INBOARD TRACK. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .50 INCH CRACK IN LOWER SKIN OF NR 5 SLAT. THE CRACK WAS LOCATED AT CORNER OF SKIN BELOW INBOARD TRACK. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3.