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 727D BETWEEN S-8R AN D S-9R HAS CRACK AT I/B FASTENER HOLE FOR AC OUTLET EXTRUSION SU PPORT BRACKET (REPAIR PER W/C SEQ #1655 FIG 3 STEP 9) COMPLETED REPAIR OF FUSELAGE FRAME @ STA 727D S8R-S9R REF ECRA 5 311-02138 & EA 5310-04716I OP1 FIG 3 (REF FLEETCYCLE N/R#9666854 FOR ALL STEPS ACCOMPLISHED)