As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT WAS FOUND WITH A SMALL CRACK AT STRINGER 22R. THE CRACK WAS REMOVED WITH A 1.1 IN X .85 IN EDGE TRIM AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 380703-14, REV A.