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 440 BETWEEN S-8L AND 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). COMPLETED REPAIR OF FUSELAGE FRAME @ STA 440 STR-8L AND STR-9L REF ECRA 5311-02138 & EA 5310-047161 OP1 FIG 3 (REF FLEETCYCLE N/ R# 9666844 FOR ALL STEPS ACCOMPLISHED)