What was found
DURING INSPECTION, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT FRAME 75 & STRINGER 2L. THE SKIN WAS REPAIRED IAW ETD 2014-145-049612.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, A CRACK WAS FOUND ON THE FUSELAGE SKIN AT FRAME 75 & STRINGER 2L. THE SKIN WAS REPAIRED IAW ETD 2014-145-049612.