As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AD/EM EO TASK - MFEC INSPECTION FOUND 01EA CRACKS APPROX 0.250" IN LENGTH FROM WL 159.00 TO WL 185.00 ON RH NOSE WHEEL WELL VERTICAL STIFFENER AS MARKED PER W/C 5312-01186-01B STEP 7. REFER TO W/C 5312-01186-02B FOR REPAIR DETAILS. (LP1318931)