As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING OFF LOADING DAMAGE TO THE MDSCD BS 1920 SUPPORT ANGLE FOUND TO BE CRACKED (REF. FIGURE 1). "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, SCHEDULE REPEAT INSPECTIONS AT EVERY 10FC AND PERMANENT REPAIR AT THE NEXT C CHECK AFTER PART 1."