What was found
(CAN) ENGINE MOUNT CRACK FOUND ON 50HR INSP. CRACK WAS FOUND IN THE LOWER LT CLUSTER PERPENDICULAR TO THE WELD RUNNING A TOTAL OF .7500" ALONG THE VERTICAL TUBE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) ENGINE MOUNT CRACK FOUND ON 50HR INSP. CRACK WAS FOUND IN THE LOWER LT CLUSTER PERPENDICULAR TO THE WELD RUNNING A TOTAL OF .7500" ALONG THE VERTICAL TUBE.