What was found
INNER FUSELAGE SKIN CORRODED AROUND DRAIN VLV BETWEEN STRINGERS 21LT & 21RT ON BOTH SIDES OF FRAME 67. REPAIRED FUSELAGE SKIN CORROSION AT FRAME 67, BETWEEN STRINGER 21LT & 21RT IAW ERS-EM-53MR-1266.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INNER FUSELAGE SKIN CORRODED AROUND DRAIN VLV BETWEEN STRINGERS 21LT & 21RT ON BOTH SIDES OF FRAME 67. REPAIRED FUSELAGE SKIN CORROSION AT FRAME 67, BETWEEN STRINGER 21LT & 21RT IAW ERS-EM-53MR-1266.