As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C 123 RUDDER LEADING EDGE ATTACH ANGLE CRACKED AT 2 RT 284.750. REMOVED CRACKED ANGLE. MATERIAL VERIFICATION PO NR 318067 7075-0.071 IAW DC8 SR M55-5-0. MATERIAL FABRICATION OF NEW ATTACH ANGLE IAW DC8 SRM 55-5-0.HEAT TREAT VERIFICATION 7075-0 TO 7075T-6 (READING 83.5) IAW TPS 1003 R EV A. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW ANGLE IAW D C8 SRM 51-3-0 & 51 -1-21.