As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE C1 DOOR SURROUND FRAME, FS 560, WEB CRACK REPAIR. A INCH 2 CRACK WAS FOUND IN THE WEB OF THE FORWARD JAMB FRAME OF THE C1 DOOR OPENING. THE CRACK WAS LOCATED AT THE 2ND FROM THE TOP DOOR STOP. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A DOUBLER PER ER/A 368008-14.