As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 0.4 CRACK IN MID CARGO DOOR FORWARD PAN LEADING EDGE SKIN UNDER FITTING (TWO INCHES ABOVE TORQUE TUBE). THE FITTING WAS REMOVED IAW SRM 51-30-5 AND THE CRACK WAS STOP DRILLED. THE DOOR PAN WAS REPAIRED AND THE FITTING WAS REINSTALLED IAW ECRA 5330-02819 AND SRM 51-30-5.