As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER BEING INSPECTED PER SI 7-69903-12AD, THE RT SIDE FUSELAGE FRAME WAS FOUND CRACKED AT THE TYPICAL LOCATION OVER THE WL 280.6 LONGERON AND DIRECTLY OVER STR 14. THE CRACK WAS REPAIRED PER THE SI WITH MINOR DEVIATIONS. REV B TO ER/A PROVIDES FAA APPROVAL.