What was found
DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 BELOW STRINGER 2L. THE STRINGER WAS REPAIRED IAW ETD 2014-145-096626.
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 BELOW STRINGER 2L. THE STRINGER WAS REPAIRED IAW ETD 2014-145-096626.