As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 4 INCH CRACK IN ANGLE AND DOUBLER AT RT WING FIXED LEADING EDGE RIB AT SLAT STA 0. THE DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND 51-40-3, FIGURE 1.