As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK INSPECTION THE FOLLOWING WAS FOUND; RT MAIN LANDING GEAR W/W STA 857 AND XCW51 PRESSURE BULKHEAD STIFFENER UPPER SECTION ANGLE WITH CRACK. DRILLED A STOP HOLE AT END OF CRACK IAW DC8 SRM 53-2-0, FABRICATED REINFORCEMENT IAW DC8 SRM 53-2-0, PRIMED REINFORCEMENT IAW DC8 SRM 51-1-8 AND INSTALLED REINFORCEMENT IAW DC8 SRM 51-1-21.