What was found
DURING INSPECTION, THE SHEAR CLIP AT FRAME 26 AND STRINGER 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP 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 SHEAR CLIP AT FRAME 26 AND STRINGER 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.