What was found
DURING 2C INSPECTION, FOUND STRINGERS IN LOWER FUSELAGE AREA BELOW LAV TO HAVE SURFACE CORROSION. CLEANED LIGHT CORROSION, TREATED AND PAINTED PER M/M 51-20-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 2C INSPECTION, FOUND STRINGERS IN LOWER FUSELAGE AREA BELOW LAV TO HAVE SURFACE CORROSION. CLEANED LIGHT CORROSION, TREATED AND PAINTED PER M/M 51-20-04.