What was found
DURING SCHEDULED SPECIAL VISIT FOR FUSELAGE SKIN LAP INSPECTION, FOUND CRACK INDICATIONS AT VERTICAL STIFFENER, BS 178, RBL 6, WL 184. 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 VERTICAL STIFFENER, BS 178, RBL 6, WL 184. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.