What was found
INSPECTION FOUND A .25 INCH CRACK AT TWO RIVETS (SIX INCHES INBOARD OF ACTUATOR) ON NR 6 LEADING EDGE SLAT. THE SLAT WAS REPAIRED IAW ECRA 5750-01159.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .25 INCH CRACK AT TWO RIVETS (SIX INCHES INBOARD OF ACTUATOR) ON NR 6 LEADING EDGE SLAT. THE SLAT WAS REPAIRED IAW ECRA 5750-01159.