What was found
DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 & STRINGER 1R. THE SKIN WAS REPAIRED IAW ETD2014-145-105115.
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 1R. THE SKIN WAS REPAIRED IAW ETD2014-145-105115.