As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT FUSELAGE CANTED FRAME AT F/A 1178 CRACKED AT LONGERON 16 LEFT. INSTALLED DOUBLER REPAIR AT LEFT HAND CANTED FRAME AT STA 1178 LONGERON 18L IAW B717 SRM 51-70311 FIG 201 PAGE 203. MATERIAL USED 0.080" 7075-0, 13 X 2.5 INCHES. HEAT TREATED TO T6 IAW AVBORNE G-PS 98PMS.247PS-01 AND SRM 51-32-01.