As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1 INCH CRACK IN STIFFENER VERTICAL ANGLE AT RT MLG WHEEL WELL REAR BULKHEAD LOWER O/B CORNER JOINT TO LONGERON TO BULKHEAD. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-35-02 AND 51-33-01, FIGURE 1.