What was found
DURING INSPECTION, CORROSION WAS FOUND ON SHEAR CLIP AT FRAME 10 BETWEEN STRINGER 21R AND 20R. THE SHEAR CLIP AT FRAME 10 WAS REPLACED IN ACCORDANCE WITH SRM 53-12-04 AND 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 SHEAR CLIP AT FRAME 10 BETWEEN STRINGER 21R AND 20R. THE SHEAR CLIP AT FRAME 10 WAS REPLACED IN ACCORDANCE WITH SRM 53-12-04 AND 51-40-02.