What was found
INSPECTION FOUND A 3 INCH CRACK ON LOWER LEADING EDGE CHORD JUST OUTBOARD OF OUTBOARD TRACK FOR NR 2 LEADING EDGE SLAT. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 3 INCH CRACK ON LOWER LEADING EDGE CHORD JUST OUTBOARD OF OUTBOARD TRACK FOR NR 2 LEADING EDGE SLAT. THE CRACK WAS STOP DRILLED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.