What was found
DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 AND STRINGER 2L. THE SKIN WAS REPAIRED IAW ETD 2015-145-059490.
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 AND STRINGER 2L. THE SKIN WAS REPAIRED IAW ETD 2015-145-059490.