What was found
INSPECTION FOUND A 1.125 INCH CRACK ABOVE NR 1 FLAP TRACK AREA IN LT WING OUTBOARD FOREFLAP LEADING EDGE. A DOUBLER WAS INSTALLED IAW SRM 57-50-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.125 INCH CRACK ABOVE NR 1 FLAP TRACK AREA IN LT WING OUTBOARD FOREFLAP LEADING EDGE. A DOUBLER WAS INSTALLED IAW SRM 57-50-4.