What was found
INSPECTION FOUND A 5/16 CRACK IN L/H WING OUTBOARD FOREFLAP LEADING EDGE ABOVE #1 SEQUENCE CARRIAGE AREA. A REPAIR WAS INSTALLED IAW SRM 57-50-4, PAGES 16 AND 17, FIGURE 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 5/16 CRACK IN L/H WING OUTBOARD FOREFLAP LEADING EDGE ABOVE #1 SEQUENCE CARRIAGE AREA. A REPAIR WAS INSTALLED IAW SRM 57-50-4, PAGES 16 AND 17, FIGURE 7.