As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ONE CRACK FOUND AT ONE TOP DYNAFOCAL WELD TO TUBE, FOUR CRACKS FOUND AT CROSS TUBE BETWEEN LOWER LEGS AT WELDED AREAS. ALL CRACKS FOUND DURING DYE-PENETRANT INSPECTION CARRIED OUT IN ACCORDANCE WITH CESSNA'S CONTINUING AIRWORTHINESS PROGRAM, CAP 71-20-00. MOUNT IS OLDER STYLE, LACKING WELDED FINGER-PATCH REINFORCEMENTS FOUND ON LATER MODELS AT CROSS-TUBE WELDS. CRACKS REPAIRED AND MOUNT RETURNED TO SERVICE.