As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND DAMAGE IN THE FORM OF MATERIAL LOSS ON EDGE OF SKIN AT LT SIDE OF FUSELAGE, BS 360 BETWEEN STRINGER 17L AND 18L, AT PRODUCTION JOINT. THE AREA WAS BLENDED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-02493 AND SRM 53-30-3.