As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A PHASE 2, 200 HR INSP, A CRACK WAS FOUND ON THE LT ENGINE MOUNT UPPER IB COWLING BRACKET. THE CRACK EXTENDED FROM THE TOP OF THE WELD AND WAS APPROXIMATELY 1 INCH IN LENGTH. THE ADJACENT AREAS DID NOT APPEAR DAMAGED.. TECH SUPPORT WAS CONTACTED AND THE MOUNT SENT TO A QUALIFIED WELDER FOR REPAIR. CAUSE OF CRACK IS UNKNOWN. (K)