What was found
INSPECTION FOUND A 2.6 INCH CRACK AT ANGLE BELOW INBOARD STOP FITTING AT NR 3 SLAT. THE CRACK WAS STOP DRILLED, AN EXTRUDED 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 2.6 INCH CRACK AT ANGLE BELOW INBOARD STOP FITTING AT NR 3 SLAT. THE CRACK WAS STOP DRILLED, AN EXTRUDED ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4.