As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 1.2 INCH CRACK IN MID CARGO DOOR AFT PAN FLANGE ADJACENT TO TORQUE TUBE CAM. THE CRACK WAS STOP DRILLED IAW SRM 52-03, FIGURE 1. THE EXISTING REPAIR DOUBLER WAS REMOVED FOR ACCESS. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A AND 51-10-3. THE EXISTING REPAIR DOUBLER WAS REINSTALLED IAW SRM 51-30-2.