What was found
INSPECTION FOUND A .5 INCH CRACK IN LT INBOARD FLAP AFT SEGMENT LEADING EDGE SKIN, 64 INCHES FROM OUTBOARD END. THE CRACKED AREA WAS REMOVED. A REPAIR ANGLE AND STRAP WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-6.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK IN LT INBOARD FLAP AFT SEGMENT LEADING EDGE SKIN, 64 INCHES FROM OUTBOARD END. THE CRACKED AREA WAS REMOVED. A REPAIR ANGLE AND STRAP WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-6.