As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) POST INSTALLATION DURING FUNCTIONAL TEST THE UNIT DISCOVERED TO BE LEAKING. AFTER REMOVAL OF THE FEEL COMPUTER IT WAS NOTICED THAT A CRACK APPROX. 3 INCHES IN LENGTH WAS WMITTING FROM THE ACTUATOR MOUNTING COVER. THE CRACK ITSELF IS LOCATED ON THE CHAMBER. THIS UNIT WAS RECENTLY OVERHAULED BY AVBORNE ACCESSORY GROUP INC.