What was found
INSPECTION FOUND A 1 INCH CRACK IN LT WING LEADING EDGE SKIN AT NR 5 LEADING EDGE SLAT INBOARD TRACK CUTOUT. REMOVED FASTENER IAW SRM 51-31-01. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-00-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN LT WING LEADING EDGE SKIN AT NR 5 LEADING EDGE SLAT INBOARD TRACK CUTOUT. REMOVED FASTENER IAW SRM 51-31-01. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-00-01.