As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING AN ANNUAL INSPECTION, CRACKS WERE FOUND AT THE ATTACHMENT POINTS OF THE ENGINE FORWARD SUPPORTS. FORWARD ENGINE LEG SUPPORTS FITTINGS AND STIFFENERS 206-031-629-103 AND 206-031-201-291 REPLACED. ENGINE MOUNT SUPPORT CHANNEL AND FRAME 206-031-302-257 REPLACED.