What was found
DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 AND STRINGER 2R. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2015-145-00367
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 2R. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2015-145-00367