What was found
INSPECTION FOUND A 1 INCH CRACK AT INBOARD AND OUTBOARD ENDS OF NR 2 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK AT INBOARD AND OUTBOARD ENDS OF NR 2 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.