What was found
DURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP & T FITTING AT FRAME 65 BETWEEN STINGERS 15L & 16L. THE SHEAR CLIP & T FITTING WERE 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, CORROSION WAS FOUND ON THE SHEAR CLIP & T FITTING AT FRAME 65 BETWEEN STINGERS 15L & 16L. THE SHEAR CLIP & T FITTING WERE REPLACED IAW SRM 51-40-02.