As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK NOTICED AFT FUSELAGE INT LEFT CANTED FRAME AREA STA 1178.225 BELOW L16L AFT OF HYD S/O VALVE. INSTALLED ANGLE REPAIR AT LEFT CANTED FRAME STA 1178.225 BELOW L161L, AFT OF HYD S/O VALVE IAW B717 SRM 51-70-11 FIG 201 REPAIR 1. MATERIAL USED 7075-0 .080 SIZE 11" X 21.2". HEAT TREATED FROM 0 TO T6 IAW AVBORNE HEAVY MAINTENANCE, GENERAL PROCESS SPEC 98PMS.24PS-01.