What was found
FUSELAGE EXTERIOR SKIN PANEL HAS CORROSION AROUND SEVERAL FASTENERS AND TWO DRAINS BETWEEN FS 559+32 AND 559+48 S26L & 26R. NO DAMAGE ALLOWED IN THIS AREA. REPAIRED IAW CL600-2B19-53-I00159.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE EXTERIOR SKIN PANEL HAS CORROSION AROUND SEVERAL FASTENERS AND TWO DRAINS BETWEEN FS 559+32 AND 559+48 S26L & 26R. NO DAMAGE ALLOWED IN THIS AREA. REPAIRED IAW CL600-2B19-53-I00159.