What was found
INSPECTION FOUND A 2 INCH CRACK AT AFT END OF LT WING LEADING EDGE SLAT STA 0 RIB UPPER ATTACH ANGLE. THE ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK AT AFT END OF LT WING LEADING EDGE SLAT STA 0 RIB UPPER ATTACH ANGLE. THE ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1.