As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON THE LOWER C-PIT DOOR CORNER PAN. REPAIRED ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION A NEW PAN AND SPLICE PLATES IN ACCORDANCE WITH DAC DRAWINGS 5707387-501, 5074349-7 AND DACO STRUCTURAL REPAIR MANUAL.