What was found
(CAN) CIRCUMFERENTIAL CRACK ON FIRST PANEL AFT OF MOUNTING BRACKET. LEFT SIDE CRACK APPROXIMATELY 1 INCH LONG. MANUFACTURER CONTACTED AND REPAIR IMPLEMENTED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) CIRCUMFERENTIAL CRACK ON FIRST PANEL AFT OF MOUNTING BRACKET. LEFT SIDE CRACK APPROXIMATELY 1 INCH LONG. MANUFACTURER CONTACTED AND REPAIR IMPLEMENTED.