As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT FUSELAGE COMPARTMENT ZONE 312 BS Y 2060 CANT, CROWN AREA, TOP SIDE CHANNEL AND LWR SIDE CLIP FOUND CRACKED. *S/D* REMOVED AND REPLACED CHANNEL AND CLIP PER SRM 51-35-01 & 51-33-01 VOL II AND DWG AJC 7372 & AJC 7029. NEW CHANNEL HEAT TREAT CARRIED OUT PER DPS 7.00-01 AND HARDNESS RESULT HRB 83 AS PER DPS 1.05-3.