What was found
FUSELAGE SKIN AT FORWARD LAV SERVICE DOOR CUTOUT LOWER EDGE CORRODED BETWEEN BS 268 TO BS 272, STR 22R. REMOVED AND REPLACED SKIN PER SRM AND DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN AT FORWARD LAV SERVICE DOOR CUTOUT LOWER EDGE CORRODED BETWEEN BS 268 TO BS 272, STR 22R. REMOVED AND REPLACED SKIN PER SRM AND DWG.