As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR PAN AT FORWARD AND AFT SIDE. THE CRACK WAS LOCATED AT RADIUS BELOW LATCH. THE CRACKS WERE STOP DRILLED IAW SRM 52-05, FIGURE 26A. REPAIR ANGLES WERE INSTALLED AT EACH LOCATION IAW SRM 52-05, FIGURE 26A.