As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT FUSELAGE COMPARTMENT LT STA 1178 CANTED FRAME CRACKED JUST BELOW L-7.L. CUT OUT DAMAGED SECTION 3.0" BY 1.0" AND INSTALLED FILLER .071" 70-75-T6 PO 021267 AND REPAIR ANGLE DOUBLER .080" 7075-0 PO NR 04721. HEAT TREATED TO T-6 PER B717 SRM 51-32-01 AND INSTALLED IAW B717 SRM 51-70-11.