What was found
INSPECTION FOUND A 2 INCH CRACK AT UPPER EDGE OF RT WING LEADING EDGE RIB, SLAT STA 0. THE CRACK WAS STOP DRILLED, A WEB REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-20-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK AT UPPER EDGE OF RT WING LEADING EDGE RIB, SLAT STA 0. THE CRACK WAS STOP DRILLED, A WEB REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-20-1.