As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING SCHEDULED INSPECTION, DISCOVERED 1.5 INCH CRACK RUNNING LONGITUDINALLY ON RIGHT SIDE OF NOSE LANDING GEAR WHEEL WELL THROUGH EXISTING FASTENER HOLES, START AND STOP. CRACK LOCATION WAS OUTSIDE THE PRESSURE VESSEL. DAMAGE AREA WAS REMOVED AND ALUMINUM FLUSH PATCH INSTALLED PER FAA DER APPROVED DATA.