As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .1875 INCH CRACK IN NLG RT SIDE PRESSURE PANEL OUT OF FASTENER HOLE AT BS 271, WL 185. THE EXISTING DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6A. A DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-2 AND MM 51-20-11.