As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND STA 285.62 NOSE WHEEL WELL RT VERTICAL STIFFENER CORRODED 3 INCHES FROM LOWER END AND 2 INCHES FROM UPPER END. THE VERTICAL STIFFENER WAS REMOVED, A REPLACEMENT STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2 AND BAC DRAWING 65-45819.