As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT FUSELAGE LT CANTED FRAME IS CRACK IN TWO PLACES AT STA 1178.225 BETWEEN L-16L TO 18L. INSTALLED DOUBLER REPAIR AT LEFT CANTED FRAME AT STA 1178.225 BETWEEN L-16L TO 18L IAW B717 SRM 51-70-01 FIG 201. MATERIAL USED 7075-080; HEAT TREATED TO T6 IAW AVBORNE G-PS 98PMS.247PS-01 AND 7075T6 SIZE OF REPAIR 15 X 4 INCHES.