What was found
INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE RIB INBOARD OF NR 4 LEADING EDGE FLAP AT LEADING EGDE STA 130. THE CRACK WAS STOP DRILLED AND AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-1, AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE RIB INBOARD OF NR 4 LEADING EDGE FLAP AT LEADING EGDE STA 130. THE CRACK WAS STOP DRILLED AND AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-1, AND 51-30-2.