As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT SUPPORT BRACKET AT FRAME 8 AND STRINGER 9R IN THE FORWARD FUSE II SECTION. MAINTENANCE REPLACED THE RIGHT FORWARD FUSELAGE II FRAME 8 ANGLE SUPPORT ABOVE STRINGER 9R IN ACCORDANCE WITH SRM 51-0-02.