As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR INNER SKIN. THE CRACK WAS LOCATED 4 FROM FORWARD EDGE AND 10 BELOW UPPER TORQUE TUBE. THE CRACKED AREA WAS CUT OUT IAW SRM 51-40-2, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 51-30-2.