What was found
CRACK IN SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 16 R AND 17 R. REMOVED CRACKED SHEAR CLIP, LOCATED DRILLED AND APPLIED ALODINE TO NEW SHEAR CLIP AND INSTALLED IAW SRM 51-40-02, 53-31-04, 51-20-03 AND CPM 51-21-04.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN SHEAR CLIP AT FRAME 24 BETWEEN STRINGERS 16 R AND 17 R. REMOVED CRACKED SHEAR CLIP, LOCATED DRILLED AND APPLIED ALODINE TO NEW SHEAR CLIP AND INSTALLED IAW SRM 51-40-02, 53-31-04, 51-20-03 AND CPM 51-21-04.