What was found
DURING INSPECTION, CORROSION AND A CRACK WAS FOUND ON THE NOSE LANDING GEAR WHEEL WELL ANGLE AT THE LEFT FORWARD CORNER. THE ANGLE WAS REPLACED IN ACCORDANCE WITH SRM 51-40-21.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, CORROSION AND A CRACK WAS FOUND ON THE NOSE LANDING GEAR WHEEL WELL ANGLE AT THE LEFT FORWARD CORNER. THE ANGLE WAS REPLACED IN ACCORDANCE WITH SRM 51-40-21.