What was found
DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 178 BULKHEAD SKIN, WL 218, RBL 10-12, AT WL 187 TO 203, AND WL 202 TO 188, RBL 5.7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT BS 178 BULKHEAD SKIN, WL 218, RBL 10-12, AT WL 187 TO 203, AND WL 202 TO 188, RBL 5.7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.