What was found
D: Center Bulkhead Web Crack At Body STA .178 . WL 187. BLO.C: Remove Crack Per SRM 53-10-08 Fig 203. NDT Checked For Crack Containment. Frabricate Repair Parts and installed Per SRM 53-10-08 Fig 203
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
D: Center Bulkhead Web Crack At Body STA .178 . WL 187. BLO.C: Remove Crack Per SRM 53-10-08 Fig 203. NDT Checked For Crack Containment. Frabricate Repair Parts and installed Per SRM 53-10-08 Fig 203