What was found
INTERNAL LOWER SKIN TO STRINGER CORROSION FOUND DURING ROUTINE INSPECTION. CORROSION LOCATED BETWEEN BONDED STRINGER 16 AND FUSELAGE SKIN, BETWEEN FS 220 AND FS 236. CORROSION APPROX. 6 INCHES TO 8 INCHES IN LENGTH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INTERNAL LOWER SKIN TO STRINGER CORROSION FOUND DURING ROUTINE INSPECTION. CORROSION LOCATED BETWEEN BONDED STRINGER 16 AND FUSELAGE SKIN, BETWEEN FS 220 AND FS 236. CORROSION APPROX. 6 INCHES TO 8 INCHES IN LENGTH.