What was found
DURING INSPECTION, THE AFT FUSELAGE INSIDE ACCESS 312AR FRAME 80 SHEAR CLIP WAS FOUND CRACKED AT STRINGER 1L. THE SHEAR CLIP WAS REPLACED IAW WITH SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, THE AFT FUSELAGE INSIDE ACCESS 312AR FRAME 80 SHEAR CLIP WAS FOUND CRACKED AT STRINGER 1L. THE SHEAR CLIP WAS REPLACED IAW WITH SRM 51-40-02.