What was found
INSPECTION FOUND A 1 INCH CRACK IN LT WING LEADING EDGE STIFFENER AT NR 4 SLAT INBOARD TRACK, STA XORS 465. THE CRACK WAS STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-00-01 AND 51-21-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN LT WING LEADING EDGE STIFFENER AT NR 4 SLAT INBOARD TRACK, STA XORS 465. THE CRACK WAS STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-00-01 AND 51-21-01.