What was found
AFTER NR ONE FLAP REMOVAL, THE NR ONE FLAP ACTUATOR WAS INSPECTED AND AN EIGHT INCH CRACK WAS FOUND RUNNING LATERAL ON THE FLAP ACTUATOR DRIVE SHAFT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER NR ONE FLAP REMOVAL, THE NR ONE FLAP ACTUATOR WAS INSPECTED AND AN EIGHT INCH CRACK WAS FOUND RUNNING LATERAL ON THE FLAP ACTUATOR DRIVE SHAFT.