As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INVESTIGATION REVEALED A BROKEN CLEVIS ON THE NOSE GEAR ACTUATOR. DURING THE GEAR CYCLE, THE BROKEN END OF THE ACTUATOR ROTATED DOWN WHILE THE NOSE GEAR SWUNG FREELY. UPON GEAR EXTENSION, THE END OF THE ACTUATOR WEDGED AGAINST A BULKHEAD WITHIN THE GEAR WELL RESTRICTING THE DEPLOYMENT OF ALL OTHER GEAR ACTUATORS. IT WAS FURTHER DETERMINED THE LOCATION OF THE CLEVIS BREAK WAS LOCATED INTERNALLY TO THE ACTUATOR SHAFT AND WOULD NOT HAVE BEEN VISIBLE DURING NORMAL INSPECTION PROCEDURES.