What was found
DURING SCHEDULED D-CHECK, FOUND CRACK IN AFT SIDE OF PRESSURE BULKHEAD FWD CHORD TO VERTICAL STIFFENER AT BS 178 WL 184 LBL 5.7 AND AT WL 184 LBL 5.7. REPAIRED PER BOEING SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED D-CHECK, FOUND CRACK IN AFT SIDE OF PRESSURE BULKHEAD FWD CHORD TO VERTICAL STIFFENER AT BS 178 WL 184 LBL 5.7 AND AT WL 184 LBL 5.7. REPAIRED PER BOEING SRM.