As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT FUSELAGE COMPARTMENT CANTED FRAME 1178 AND LEFT HAND LONGERON 17, AREA HAS CRACK. CUT OUT DAMAGE ON CANTED FRAME STA 1178 LEFT SIDE L-17L TO 18L (2.5 X 1.375 INCHES) IAW B717 SRM 51-70-11 FIG 201. FABRICATED REPAIR ANGLE AND FILLER MATERIAL USED 7075. T6 .080 11 X 2.5 INCHES. PO 021701. HEAT TREATMENT TO T-6 IAW 98 PMS 247 OS 01 AS PER SRM 51-30-01.