What was found
INSPECTION FOUND A .5 INCH CRACK IN O/B LOWER END OF SUPPORT BRACKET WHERE LT WING NR 1 L/E FLAP ACTUATOR MOUNTS INSIDE LEADING EDGE. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2 AND 51-20-2 FIGURE 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN O/B LOWER END OF SUPPORT BRACKET WHERE LT WING NR 1 L/E FLAP ACTUATOR MOUNTS INSIDE LEADING EDGE. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2 AND 51-20-2 FIGURE 7.