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; 4TH 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 PO 606256.4. FABRICATED STIFFENER IAW DAC DWG ANB 7203, REV "BA". ALODINED; PRIMER AND PAINTED IAW DC/MD-10 SRM 51-21-01, PGS 21-24 AND 51-21-02; VOL II. INSTALLED STIFFENER IAE DC/MD-10 SRM 51-35-01; AND 51-33-01; VOL II.