What was found
DURING INSPECTION THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 & STRINGER 2R. THE SKIN WAS REPAIRED IAW ETD 2014-145-086559.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 & STRINGER 2R. THE SKIN WAS REPAIRED IAW ETD 2014-145-086559.