What was found
DURING SCHEDULED C-11 CHECK, FOUND THE LT AFT FUSELAGE INTERIOR FS880 BULKHEAD WEB HAD CRACKED AT WL 200, LBL66. REPAIR BY WEB REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60, 51-70 AND 51-140-17. NR 2102.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C-11 CHECK, FOUND THE LT AFT FUSELAGE INTERIOR FS880 BULKHEAD WEB HAD CRACKED AT WL 200, LBL66. REPAIR BY WEB REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60, 51-70 AND 51-140-17. NR 2102.