What was found
DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 ABOVE STRINGER 2L. THE STRINGER WAS REPLACED IAW SRM 51-40-02.
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 ABOVE STRINGER 2L. THE STRINGER WAS REPLACED IAW SRM 51-40-02.