As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT MLG WHEEL WELL; LEFT WING INBD WEB 2ND AFT ANGLE AFT OF THE MLG CUTOUT IS CRACKED. REMOVED STIFFENER IAW DC/MD-10 SRM 51-35-01 AND 51-33-01; VOL II. MATERIAL ID FOR THE STIFFENER 7075-0, 0.040. FABRICATED STIFFENER IAW DAC DWG ANB 7208, REV "AB". ALODINED; PRIMED AND PAINTED IAW DC/MD-10 SRM 51-21-01; PGS 21-24 AND 51-21-02; VOL II. INSTALLED THE STIFFENER IAW DC/MD-10 SRM 51-35-01 AND 51-33-01; VOL II.