What was found
FUSELAGE INTERNAL SKIN CORRODED, BS 2080-2100 STR 35-36R AT LAVATORY VENT EXHAUST. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL DOUBLER & TRIPLER.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE INTERNAL SKIN CORRODED, BS 2080-2100 STR 35-36R AT LAVATORY VENT EXHAUST. MAJOR REPAIR ACCOMPLISHED: INSTALLED EXTERNAL DOUBLER & TRIPLER.