What was found
(CAN) THIS LT FLAP COANTROL ARM WAS FOUND CRACKED DURING AN INSPECTION. THE CRACK WAS 188 MM/0.7 INCH RUNNING LENGTHWISE FROM THE THREADED END OF THE ROD ENDING AT THE INSPECTION HOLE. THIS PART WAS REPLACED WITH A NEW UNIT.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) THIS LT FLAP COANTROL ARM WAS FOUND CRACKED DURING AN INSPECTION. THE CRACK WAS 188 MM/0.7 INCH RUNNING LENGTHWISE FROM THE THREADED END OF THE ROD ENDING AT THE INSPECTION HOLE. THIS PART WAS REPLACED WITH A NEW UNIT.