As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .125 INCH CRACK IN TOP RIGHT PANEL OF NOSE WHEEL WELL AT FS 269, RBL 10. THE FASTENERS WERE REMOVED IAW SRM 51-30-2. THE CRACKED AREA WAS CUT OUT IAW EA 5362-01016. DOUBLER, STRAP, AND FILLER WERE FABRICATED AND INSTALLED IAW EA 5362-01016 AND SRM 51-10-2.