What was found
FUSELAGE INTERNAL SKIN BETWEEN FRAME 13 & 14, STRINGER 21R & 19R IS CORRODED. PERFORMED REPAIR IAW ERS-EM-53MR-829.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE INTERNAL SKIN BETWEEN FRAME 13 & 14, STRINGER 21R & 19R IS CORRODED. PERFORMED REPAIR IAW ERS-EM-53MR-829.