What was found
FUSELAGE LOWER BODY FAIRING PANEL HAS CORROSION. REMOVED CORROSION, APPLIED FILLER, APPLIED CONDUCTIVE COATING, PRIMED AND PAINTED PER SRM 51-10-01, 51-40-08, 51-24-17.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE LOWER BODY FAIRING PANEL HAS CORROSION. REMOVED CORROSION, APPLIED FILLER, APPLIED CONDUCTIVE COATING, PRIMED AND PAINTED PER SRM 51-10-01, 51-40-08, 51-24-17.