What was found
INSPECTION FOUND A 1 INCH CRACK IN NR 2 LEADING EDGE SLAT FIRST RIB INBOARD OF ACTUATOR AT WS 629. A FORMED ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN NR 2 LEADING EDGE SLAT FIRST RIB INBOARD OF ACTUATOR AT WS 629. A FORMED ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-0.