What was found
LEVEL 2 CORROSION, FUSELAGE LOWER LOBE SKIN IS CORRODED AT CENTER PRESSURE BULKHEAD VERTICAL SUPPORT 4 INCHES LBL BETWEEN BS 1606 AND 1585. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEVEL 2 CORROSION, FUSELAGE LOWER LOBE SKIN IS CORRODED AT CENTER PRESSURE BULKHEAD VERTICAL SUPPORT 4 INCHES LBL BETWEEN BS 1606 AND 1585. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2. (W)