What was found
CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN FRAMES 60 - 61, STRINGER 20 - 21L. REPAIRED THE SKIN.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON INTERNAL FUSELAGE SKIN BETWEEN FRAMES 60 - 61, STRINGER 20 - 21L. REPAIRED THE SKIN.