What was found
LOWER FUSELAGE ACCESS PANEL 192BB & 191BB CENTER NUTPLATE CHANNEL CORRODED IN SEVERAL AREAS. BLENDED CORROSSION FROM CENTER TEE CHANNEL STRUCTURE REF 51-12-00-001-001-A01. DAMAGE BEYOND ALLOWABLE LIMIS IAW SRM 53-82-55-101-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER FUSELAGE ACCESS PANEL 192BB & 191BB CENTER NUTPLATE CHANNEL CORRODED IN SEVERAL AREAS. BLENDED CORROSSION FROM CENTER TEE CHANNEL STRUCTURE REF 51-12-00-001-001-A01. DAMAGE BEYOND ALLOWABLE LIMIS IAW SRM 53-82-55-101-001-A01.