What was found
INSPECTION FOUND A .875 INCH AND .25 INCH CRACK IN LT OUTBOARD FOREFLAP LEADING EDGE CUTOUT ABOVE NR 1 FLAP TRACK. THE FLAP WAS REPAIRED IAW SRM 57-50-4, FIGURE 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .875 INCH AND .25 INCH CRACK IN LT OUTBOARD FOREFLAP LEADING EDGE CUTOUT ABOVE NR 1 FLAP TRACK. THE FLAP WAS REPAIRED IAW SRM 57-50-4, FIGURE 1.