What was found
INSPECTION FOUND A 1.5 INCH CRACK IN RADIUS OF ANGLE AT INBOARD UPSTOP BLOCK ON NR 7 LEADING EDGE SLAT. THE CRACKED ANGLE WAS REMOVED AND NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2.
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 RADIUS OF ANGLE AT INBOARD UPSTOP BLOCK ON NR 7 LEADING EDGE SLAT. THE CRACKED ANGLE WAS REMOVED AND NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2.