What was found
INSPECTION FOUND TWO VERTICAL STIFFENER ANGLES ON LT WHEEL WELL AFT SIDE WEB CRACKED. THE CRACKS WERE .5 INCH LONG. THE TWO ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND TWO VERTICAL STIFFENER ANGLES ON LT WHEEL WELL AFT SIDE WEB CRACKED. THE CRACKS WERE .5 INCH LONG. THE TWO ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-31-01.