What was found
FUSELAGE SKIN CORRODED AROUND OPENING OF LAV VACUUM MOTOR EXHAUST PORT. FOUND INTERNAL BRACKET CORRODED BEYOND SRM LIMITS. R & R BRACKET IAW DWG 5936667.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CORRODED AROUND OPENING OF LAV VACUUM MOTOR EXHAUST PORT. FOUND INTERNAL BRACKET CORRODED BEYOND SRM LIMITS. R & R BRACKET IAW DWG 5936667.