As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT CANTED FRAME IS CRACKED, AFT FUSELAGE SECTION. INSTALLED REPAIR ON LEFT HAND CANTED FRAME AT STA 1178 BETWEEN LONG 16 AND L17, IAW B717 SRM 51-70-11L. MATERIAL USED FILLER 7075-T6-.071 X 1" DOUBLER 7075.0.080 9" X 1" X 1.25". HEAT TREATED TO 7075-T6.080 PER GPS 98PMS.247PS-01.