What was found
FUSELAGE SKIN CORRODED BETWEEN BS 360 TO BS 540, BETWEEN STR 14L TO STR 24L. REPAIRED SKIN PER SRM AND DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CORRODED BETWEEN BS 360 TO BS 540, BETWEEN STR 14L TO STR 24L. REPAIRED SKIN PER SRM AND DWG.