As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L-SHAPED CRACK AROUND 0.50 X 0.75" PLUS DENT BETWEEN RUDDER STA 131.108 AND 156.031. 620MM FROM REAR SPAR AND 290MM FROM T/E 485MM FROM FROM ACTUATOR RIB FASTENER LINE STA 165.074 AND 725MM FROM ACTUATOR RIB FASTENER LINE STA 115.142. ACCOMPLISHED PERMANENT REPAIR IAW EO B767-5540-47256-A, SRM 55-40-01-2R AND SRM 51-70-17.TRIM OUT FINAL 1.18" IN DIAMETER.