As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NOSE WHEEL WELL, LT SIDEWALL STIFFENER BETWEEN FUSELAGE STATION 320 LT AND 340 LT, WL 180, WAS FOUND WITH CRACK DURING HFEC INSPECTION. REMOVED AND REPLACED STIFFENER WITH A NEW STIFFENER EXTRUSION P/N BAC1517-1558 IAW SRM 51-40-04 FIG. 2 AND SRM 51-30-02.