What was found
INSPECTION FOUND LEADING EDGE OF LEFT OUTBOARD FOREFLAP SKIN CRACKED AND GALLED IN TWO PLACES AT OUTBOARD SEQUENCE CARRIAGE POSITION. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-4.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND LEADING EDGE OF LEFT OUTBOARD FOREFLAP SKIN CRACKED AND GALLED IN TWO PLACES AT OUTBOARD SEQUENCE CARRIAGE POSITION. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-4.