As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN CABIN UPPER LOBE FUSELAGE FRAME AT STA.480 BETWEEN S-8L/S- 9L HAS CRACK AT I/B FASTENER HOLE FOR AC OUTLET EXTRUSION SUPPORT BRACKET (REPAIR PER W/C SEQ#1655 FIG. 3 STEP 9) REPAIRED MAIN CABIN UPPER LOBE FUSELAGE FRAME AT STA 480 BETWEEN S-8L & S-9L IN REF TO EA5310-04716 REV 1 AND EC/RA#5311-02138 REV A SEE FLEETCYCLE N/R#9666845 FOR ALL STEPS ACCOMPLISHED.