What was found
INSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE SKIN FORWARD OF OUTBOARD SLAT CARRIAGE, NR 5 SLAT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 57-30-4, FIG 4 AND 9, MM 51-20-11.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE SKIN FORWARD OF OUTBOARD SLAT CARRIAGE, NR 5 SLAT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 57-30-4, FIG 4 AND 9, MM 51-20-11.