As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING COMPLIANCE OF THE 15,000 RECURRING STRUCTURAL INSPECTION, A CRACK WAS FOUND IN THE RIGHT FUSELAGE FRAME AT FS 207.125, AT APPROXIMATELY WL 99.0. THE CRACK WAS APPROXIMATELY .75 INCH LONG AND STARTS AT A PEAR SHAPED LIGHTENING HOLE AND EXTENDS IN AN UPWARD DIRECTION.