As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN BETWEEN BS 740 - 760, STRINGER 19R LONGITUDINAL LAP SPLICE HAS CORROSION. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW ERA 548015-14 REV O. CUT OUT DAMAGE AREA AND FOUND TO BE OUT OF LIMITS ON 00042 IAW ERA 548015-14 REV O, FABRICATED REPAIR AND INSTALLED IAW ERA 548015-14 REV O.