What was found
INSPECTION FOUND A 1.5 INCH CRACK IN INBOARD SUPPORT ANGLE AT UPPER SURFACE OF COVER BELOW LT WING NR 2 SLAT ACTUATOR. THE ANGLE WAS REMOVED AND A NEW ANGLE 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 1.5 INCH CRACK IN INBOARD SUPPORT ANGLE AT UPPER SURFACE OF COVER BELOW LT WING NR 2 SLAT ACTUATOR. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3.