As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A .5 INCH CRACK WAS FOUND IN THE WEB OF THE C1 DOOR OPENING AFT FRAME (FS 620) JUST BELOW THE NR 6 DOOR STOP. THE CRACK WAS COMMON TO A FASTENER HOLE ATTACHING THE WEB TO THE OUTER FRAME CHORD. THE WEB WAS LOCALLY TRIMMED AWAY TO REMOVE THE CRACK AND REPAIRED WITH A TITANIUM DOUBLER PER ER/A 377272-14AD.