What was found
INSPECTION FOUND A .3125 INCH CRACK AT RT OUTBOARD FOREFLAP LOWER LEADING EDGE SKIN ABOVE NR 7 FLAP TRACK AREA, 54 INCHES FROM INBOARD END. A DOUBLER WAS INSTALLED IAW SRM 57-50-4, FIGURE 1, 51-10-6, AND 51-10-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .3125 INCH CRACK AT RT OUTBOARD FOREFLAP LOWER LEADING EDGE SKIN ABOVE NR 7 FLAP TRACK AREA, 54 INCHES FROM INBOARD END. A DOUBLER WAS INSTALLED IAW SRM 57-50-4, FIGURE 1, 51-10-6, AND 51-10-2.