As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A CRACK IN LT MLG WHEEL WELL UPPER PRESSURE WEB AT LT FORWARD CORNER JUST AFT OF STA 664. LENGTH OF CRACK NOT IDENTIFIED. THE WEB WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, AND 53-10-2, FIGURE 3.